This document is the preface and contents section of the solutions manual for the textbook "Heating, Ventilating and Air Conditioning: Analysis and Design, Sixth Edition". It provides solutions to the problems in chapters 1 through 15 of the textbook. Many problems have multiple acceptable solutions. The difficulty level of problems varies significantly. Computer software is encouraged for solving many of the problems. The authors have tried to eliminate errors but some may remain and corrections are welcomed.
This document provides calculations of moisture properties for air at different temperatures and pressures. It calculates humidity ratio, enthalpy, specific volume, partial pressures and density for air at various conditions, including:
- Saturated air at 70F and 20F
- Air in a room at 22C and 50% relative humidity
- Atmospheric pressure from sea level to 6000ft and 1600m
- Enthalpy of moist air at various temperatures, pressures and elevations
- Whether moisture will condense on a window at different temperatures
- Mass flow rate of dry air in a duct at varying conditions
This document appears to be the introduction or cover page of a lab manual for a Heat Transfer lab course. It provides information about the university and engineering college where the course is taught, and lists the name and identification information for the student. It also lists the experiments that will be conducted in the lab course, including determining thermal conductivity, studying heat exchangers, measuring emissivity, and analyzing heat transfer through fins, composite walls, and during convection. The document provides an overview of the lab course and experiments but no detailed information.
This document contains information about the Carnot vapor cycle and the simple Rankine cycle. It defines the key processes in each cycle, compares ideal cycles to actual cycles, and provides examples of calculating efficiency, work, heat transfer, and other parameters for steady-flow Carnot and Rankine cycles using water as the working fluid. The document emphasizes that actual vapor power cycles involve friction, pressure drops, and heat losses not present in idealized cycles.
A rotary dryer is used to dry sand with the following specifications:
- Wet sand at 30°C with 7% moisture is dried to 0.5% moisture at 115°C.
- 20 metric tons of dried sand is produced per hour.
- Bunker oil at 41870 kJ/kg HHV is used as fuel with an efficiency of 60%.
Calculating the heat requirements and fuel consumption rate, 204 kg/hr of bunker oil is needed, equivalent to 227 liters/hr.
[W f stoecker]_refrigeration_and_a_ir_conditioning_(book_zz.org)Mike Mentzos
- The document describes thermal principles and psychrometric concepts.
- It provides solutions to example problems involving state changes of water, heat transfer calculations, psychrometric chart readings, and enthalpy/humidity ratio determinations.
- Key concepts covered include the use of steam tables, Bernoulli's equation, psychrometric equations, and heat transfer relationships for convection and radiation.
1. The report analyzes heat exchange properties of small scale Stirling engines through experiments testing different materials for heat exchangers, working fluids, and the addition of fins.
2. The experiments found that copper heat exchangers performed best at higher temperatures, and that the working fluid helium produced higher engine performance than air or carbon dioxide.
3. The addition of fins to the engine provided no significant benefit to performance in low temperature Stirling engines.
The document discusses gas turbine power plants. It describes the key components of a gas turbine - the air compressor, diffuser, combustion chamber, and turbine. Gas turbines operate using the Brayton cycle and can be open or closed cycle. They have higher efficiency than steam plants but require specialized alloys due to high operating temperatures. Major applications include aviation, power generation, oil and gas industries, and marine propulsion.
6th ed solution manual---fundamentals-of-heat-and-mass-transferRonald Tenesaca
This document contains 10 problems related to heat transfer by conduction. Each problem provides known information such as materials, dimensions, temperatures, and heat transfer rates. The problems then ask the reader to find unknown values like heat fluxes, surface temperatures, or thicknesses using Fourier's Law of heat conduction and assumptions of one-dimensional and steady-state heat transfer. The problems cover a variety of applications including insulation, walls, windows, refrigeration, and cooking.
This document provides calculations of moisture properties for air at different temperatures and pressures. It calculates humidity ratio, enthalpy, specific volume, partial pressures and density for air at various conditions, including:
- Saturated air at 70F and 20F
- Air in a room at 22C and 50% relative humidity
- Atmospheric pressure from sea level to 6000ft and 1600m
- Enthalpy of moist air at various temperatures, pressures and elevations
- Whether moisture will condense on a window at different temperatures
- Mass flow rate of dry air in a duct at varying conditions
This document appears to be the introduction or cover page of a lab manual for a Heat Transfer lab course. It provides information about the university and engineering college where the course is taught, and lists the name and identification information for the student. It also lists the experiments that will be conducted in the lab course, including determining thermal conductivity, studying heat exchangers, measuring emissivity, and analyzing heat transfer through fins, composite walls, and during convection. The document provides an overview of the lab course and experiments but no detailed information.
This document contains information about the Carnot vapor cycle and the simple Rankine cycle. It defines the key processes in each cycle, compares ideal cycles to actual cycles, and provides examples of calculating efficiency, work, heat transfer, and other parameters for steady-flow Carnot and Rankine cycles using water as the working fluid. The document emphasizes that actual vapor power cycles involve friction, pressure drops, and heat losses not present in idealized cycles.
A rotary dryer is used to dry sand with the following specifications:
- Wet sand at 30°C with 7% moisture is dried to 0.5% moisture at 115°C.
- 20 metric tons of dried sand is produced per hour.
- Bunker oil at 41870 kJ/kg HHV is used as fuel with an efficiency of 60%.
Calculating the heat requirements and fuel consumption rate, 204 kg/hr of bunker oil is needed, equivalent to 227 liters/hr.
[W f stoecker]_refrigeration_and_a_ir_conditioning_(book_zz.org)Mike Mentzos
- The document describes thermal principles and psychrometric concepts.
- It provides solutions to example problems involving state changes of water, heat transfer calculations, psychrometric chart readings, and enthalpy/humidity ratio determinations.
- Key concepts covered include the use of steam tables, Bernoulli's equation, psychrometric equations, and heat transfer relationships for convection and radiation.
1. The report analyzes heat exchange properties of small scale Stirling engines through experiments testing different materials for heat exchangers, working fluids, and the addition of fins.
2. The experiments found that copper heat exchangers performed best at higher temperatures, and that the working fluid helium produced higher engine performance than air or carbon dioxide.
3. The addition of fins to the engine provided no significant benefit to performance in low temperature Stirling engines.
The document discusses gas turbine power plants. It describes the key components of a gas turbine - the air compressor, diffuser, combustion chamber, and turbine. Gas turbines operate using the Brayton cycle and can be open or closed cycle. They have higher efficiency than steam plants but require specialized alloys due to high operating temperatures. Major applications include aviation, power generation, oil and gas industries, and marine propulsion.
6th ed solution manual---fundamentals-of-heat-and-mass-transferRonald Tenesaca
This document contains 10 problems related to heat transfer by conduction. Each problem provides known information such as materials, dimensions, temperatures, and heat transfer rates. The problems then ask the reader to find unknown values like heat fluxes, surface temperatures, or thicknesses using Fourier's Law of heat conduction and assumptions of one-dimensional and steady-state heat transfer. The problems cover a variety of applications including insulation, walls, windows, refrigeration, and cooking.
Combustion involves the rapid oxidation of a fuel with oxygen, releasing heat and combustion products. There are three main types of fuel: solid, liquid, and gaseous. Hydrocarbons are the main components of fuel and can have chain or ring structures and be saturated or unsaturated. Complete combustion fully oxidizes the fuel, while incomplete combustion leaves behind pollutants like carbon monoxide and soot. The combustion reaction requires a specific amount of oxygen that is supplied by theoretical air. Excess air is sometimes used to ensure full combustion. Emissions are released as byproducts of combustion and include nitrogen oxides, carbon monoxide, volatile organic compounds, and particulate matter.
The document discusses gas turbine cycles and thermodynamic cycles used in gas turbines. It begins by describing air standard cycles and assumptions made, including the working fluid behaving as an ideal gas. It then discusses the Otto cycle which models spark ignition engines and the processes involved. Details of the Otto cycle calculation are provided. The document also discusses the diesel cycle which models compression ignition engines and provides cycle calculations. Other topics covered include mean effective pressure, engine terminology, gas turbine components and cycles like the Brayton cycle.
This document contains a 16 question multiple choice mechanical engineering review problem set. It covers topics including: specific weight calculations, changes in weight due to elevation, pressure and force calculations for scuba diving, determining height using barometer readings, properties of gas mixtures, heat transfer between materials, gas turbine processes, combustion calculations, and thermodynamic processes including changes in temperature, pressure, volume, entropy and heat/work.
Solution for Engineering Mechanics Dynamics (6th Edition) - J. L. Meriam, L. ...shayangreen
The document provides information about Konkur exam preparation resources available on the websites www.konkur.in and Forum.konkur.in. It states that on these websites students can find answers to all their exam-related questions for all levels of educational qualifications related to the Konkur exam. The document also contains multiple repetitions of copyright information.
simple pendulum and compound pendulum | vaibration | u.o.b | Saif al-din ali
saif aldin ali madi
سيف الدين علي ماضي
s96aif@gmail.com
In this laboratory practice the simulation of a simple pendulum was
carried out with the objective of determining the acceleration of gravity
and its uncertainty, through the data obtained in the simulation. In this
one was made the assembly of a simple pendulum through a rope, a
weight, a grader and the base for pendulums, which allowed us to
obtain through the following instruments rule and timer, data as the time
in which 20 oscillations are completed and the length of the pendulum,
taking into account the uncertainties of each instrument, these data
were organized into tables and then used in the realization of graphs
expressing the time as a function of the length of the pendulum, in
addition to calculating the acceleration of gravity and its uncertainty.
The document discusses the ideal reheat Rankine cycle power plant system. It aims to reduce moisture content in steam by reheating it between turbine stages. This allows using higher boiler pressures without moisture issues in later turbine stages. Key points include reheat improving efficiency by about half compared to first reheat. Double reheat is common in supercritical pressure plants. Steam should not expand deep into the two-phase region before reheating. Optimum reheat pressure is one-fourth to one-fifth of maximum cycle pressure. Benefits include very high heat addition and efficiency. Disadvantages include increased material and initial costs. Sample problems calculate efficiency and mass flow rates for given ideal reheat cycles.
Solution Manual – Heat and Mass Transfer: Fundamentals and Application, 5th e...kl kl
Solution Manual – Heat and Mass Transfer: Fundamentals and Application, 5th edition
Author: Yunus A. Cengel, Afshin J. Ghajar
Publisher: McGraw-Hill Education
ISBN of textbook: 978-007-339818-1
The objective of this experiment is to calculate the rate of the heat transfer log mean temperature difference, and the overall heat transfer coefficient in case of Counter flow
Introduction to chemical engineering thermodynamics, 6th ed [solution]Pankaj Nishant
This document contains solutions to math problems involving concepts of thermodynamics, including calculations of work, heat, internal energy, enthalpy, and phase changes. Problem 1 calculates the work done in lifting a mass and the resulting internal energy change. Problem 2 determines the heat transferred and final temperature when water gains a small amount of heat. Problem 3 is a series of thermodynamic steps where the initial and final internal energies must sum to zero.
This document calculates the efficiency of a rotary screw compressor at a nitrogen PSA plant. It defines the polytropic coefficient and uses the ideal gas law to determine compressor power based on suction and discharge parameters. The compressor power, electrical power input, and assumed mechanical losses are used to calculate the compressor efficiency in two different ways, both resulting in an efficiency of approximately 60%.
The document summarizes Chapter 7 of a textbook on thermodynamics. It includes in-text concept questions, concept problems, sections on heat engines/refrigerators, the second law and processes, Carnot cycles and absolute temperature, finite temperature heat transfer, and ideal gas Carnot cycles. It also includes review problems at the end. The chapter examines concepts related to heat engines, refrigerators, the second law of thermodynamics, and Carnot cycles.
Engineering mechanics dynamics (6th edition) j. l. meriam, l. g. kraigeshayangreen
This document discusses the history and development of paper money. It explains that originally paper money was developed as a way to represent gold and silver coins to make large transactions more convenient. Over time, governments began to print paper money that was not backed by precious metals, which led to inflation. The document outlines some of the challenges faced by governments in managing paper currency.
This document provides thermodynamic and transport property data for several common fluids including water, steam, refrigerants, and gases. It includes tables of saturated liquid and vapor properties such as specific volume, enthalpy, and entropy. Additional tables provide properties for superheated steam, supercritical fluids, and gases at various pressures and temperatures. The document aims to serve as a reference for engineers and scientists working with these important industrial fluids.
Mechanics of materials 9th edition goodno solutions manualKim92736
This document contains solutions to problems from Chapter 2 of the 9th Edition Mechanics of Materials textbook by Goodno. It lists over 300 problems from sections 2.2 through 2.12 that have been solved, along with the full textbook reference and a link to download the full solutions manual PDF. The problems cover topics in stress, strain, Hooke's law, axial loading, torsion, shear stresses, and more.
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copyIbrahim AboKhalil
This document discusses the Brayton cycle, which is the ideal gas turbine cycle. It covers:
1. The basic components and processes of the Brayton cycle, including constant pressure heat addition, isentropic expansion, and constant pressure heat rejection.
2. Key assumptions used in analyzing the cycle, such as treating air as an ideal gas and replacing combustion with heat addition.
3. Performance parameters like thermal efficiency as a function of pressure ratio and the impact of limiting turbine inlet temperatures.
4. Modifications to improve efficiency, including regeneration which recovers heat from the exhaust to preheat the compressor inlet air.
Solution manual internal combstion engine by willard w. pulkrabekDarawan Wahid
The document discusses the benefits of exercise for mental health. It states that regular exercise can help reduce anxiety and depression and improve mood and cognitive function. Exercise causes chemical changes in the brain that may help alleviate symptoms of mental illnesses.
This document repeats the same copyright statement multiple times. The statement says that excerpts from this work (a solution manual) may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation requires permission under the 1976 United States Copyright Act.
Este documento resume algunos conceptos clave en el diseño aerodinámico de planeadores. Explora cómo los diseñadores deben encontrar un equilibrio entre baja resistencia a altas velocidades y alta sustentación a bajas velocidades. También discute la importancia del número de Reynolds, la forma del ala, los perfiles aerodinámicos y el control de pérdida. El objetivo general es minimizar la resistencia y maximizar la sustentación en diferentes regímenes de vuelo.
The document discusses a website that provides free university textbooks and solutions manuals. It states that the solutions manuals contain step-by-step solutions to all the problems in the textbooks. It invites visitors to download the textbooks and solutions manuals for free.
Arizona State University Department of Physics PHY 132 –.docxjustine1simpson78276
Arizona State University
Department of Physics
PHY 132 – University Physics Lab II – Section #: 30531
TA – Alan Moran
Lab 3
Capacitors
Submitted by:
Charles Foxworthy
6 April 2015
Abstract: This lab focuses on experimenting with parallel plate capacitors. The first part of the
lab uses a test set up that allows the user to vary the surface area and the separation of plates in
a capacitor. When the plate was its smallest (100mm2) and furthest apart (10.0mm) it yielded its
lowest capacitance (0.04 pF). The first experiment demonstrated that insertion of a dielectric
increases capacitance, using a constant sized capacitor of 250mm2, with a constant separation of
7mm a dielectric was inserted and capacitance increase to 5 times its original value to 0.79pF.
Then a new dielectric was inserted and slow removed and the capacitance decreased as
expected.
Part 2 and 3 of the experiment focused on parallel and series circuits with only switches and
capacitors. The first experiment was parallel capacitors and it demonstrated that charge was
conserved and that it was additive when capacitors are parallel. Part 3 had a capacitor in
parallel with other capacitors in series. It demonstrated that charge is constant among
capacitors that are in series, and reiterated that charge is additive when capacitors are parallel.
Both experiments had an initial charge of 0.9 and that charge stayed constant throughout the
experiments.
When it was all done the theoretical values matched the experimental values and all the
experiments were successful, and the hypotheses were proven.
Objectives: 2
Procedure: ...................................................................................................................................... 3
Experimental Data: ....................................................................................................................... 15
Results: .......................................................................................................................................... 17
Discussion and Analysis: .............................................................................................................. 19
Conclusion: ................................................................................................................................... 20
1
Objective:
The purpose of this experiment is to explore capacitors. The first experiment focuses on air gap
capacitors, and exploring changes based on a bigger gap, and/or smaller plates. The second part
to that experiment adds a nonconductive material to see the effect on the capacitance. The third
part of the experiment adds a nonconductive material and slowly removes it from the capacitor
and shows its effects. The second experiment uses capacitors in parallel and charges one then
removes the power source and ch.
Combustion involves the rapid oxidation of a fuel with oxygen, releasing heat and combustion products. There are three main types of fuel: solid, liquid, and gaseous. Hydrocarbons are the main components of fuel and can have chain or ring structures and be saturated or unsaturated. Complete combustion fully oxidizes the fuel, while incomplete combustion leaves behind pollutants like carbon monoxide and soot. The combustion reaction requires a specific amount of oxygen that is supplied by theoretical air. Excess air is sometimes used to ensure full combustion. Emissions are released as byproducts of combustion and include nitrogen oxides, carbon monoxide, volatile organic compounds, and particulate matter.
The document discusses gas turbine cycles and thermodynamic cycles used in gas turbines. It begins by describing air standard cycles and assumptions made, including the working fluid behaving as an ideal gas. It then discusses the Otto cycle which models spark ignition engines and the processes involved. Details of the Otto cycle calculation are provided. The document also discusses the diesel cycle which models compression ignition engines and provides cycle calculations. Other topics covered include mean effective pressure, engine terminology, gas turbine components and cycles like the Brayton cycle.
This document contains a 16 question multiple choice mechanical engineering review problem set. It covers topics including: specific weight calculations, changes in weight due to elevation, pressure and force calculations for scuba diving, determining height using barometer readings, properties of gas mixtures, heat transfer between materials, gas turbine processes, combustion calculations, and thermodynamic processes including changes in temperature, pressure, volume, entropy and heat/work.
Solution for Engineering Mechanics Dynamics (6th Edition) - J. L. Meriam, L. ...shayangreen
The document provides information about Konkur exam preparation resources available on the websites www.konkur.in and Forum.konkur.in. It states that on these websites students can find answers to all their exam-related questions for all levels of educational qualifications related to the Konkur exam. The document also contains multiple repetitions of copyright information.
simple pendulum and compound pendulum | vaibration | u.o.b | Saif al-din ali
saif aldin ali madi
سيف الدين علي ماضي
s96aif@gmail.com
In this laboratory practice the simulation of a simple pendulum was
carried out with the objective of determining the acceleration of gravity
and its uncertainty, through the data obtained in the simulation. In this
one was made the assembly of a simple pendulum through a rope, a
weight, a grader and the base for pendulums, which allowed us to
obtain through the following instruments rule and timer, data as the time
in which 20 oscillations are completed and the length of the pendulum,
taking into account the uncertainties of each instrument, these data
were organized into tables and then used in the realization of graphs
expressing the time as a function of the length of the pendulum, in
addition to calculating the acceleration of gravity and its uncertainty.
The document discusses the ideal reheat Rankine cycle power plant system. It aims to reduce moisture content in steam by reheating it between turbine stages. This allows using higher boiler pressures without moisture issues in later turbine stages. Key points include reheat improving efficiency by about half compared to first reheat. Double reheat is common in supercritical pressure plants. Steam should not expand deep into the two-phase region before reheating. Optimum reheat pressure is one-fourth to one-fifth of maximum cycle pressure. Benefits include very high heat addition and efficiency. Disadvantages include increased material and initial costs. Sample problems calculate efficiency and mass flow rates for given ideal reheat cycles.
Solution Manual – Heat and Mass Transfer: Fundamentals and Application, 5th e...kl kl
Solution Manual – Heat and Mass Transfer: Fundamentals and Application, 5th edition
Author: Yunus A. Cengel, Afshin J. Ghajar
Publisher: McGraw-Hill Education
ISBN of textbook: 978-007-339818-1
The objective of this experiment is to calculate the rate of the heat transfer log mean temperature difference, and the overall heat transfer coefficient in case of Counter flow
Introduction to chemical engineering thermodynamics, 6th ed [solution]Pankaj Nishant
This document contains solutions to math problems involving concepts of thermodynamics, including calculations of work, heat, internal energy, enthalpy, and phase changes. Problem 1 calculates the work done in lifting a mass and the resulting internal energy change. Problem 2 determines the heat transferred and final temperature when water gains a small amount of heat. Problem 3 is a series of thermodynamic steps where the initial and final internal energies must sum to zero.
This document calculates the efficiency of a rotary screw compressor at a nitrogen PSA plant. It defines the polytropic coefficient and uses the ideal gas law to determine compressor power based on suction and discharge parameters. The compressor power, electrical power input, and assumed mechanical losses are used to calculate the compressor efficiency in two different ways, both resulting in an efficiency of approximately 60%.
The document summarizes Chapter 7 of a textbook on thermodynamics. It includes in-text concept questions, concept problems, sections on heat engines/refrigerators, the second law and processes, Carnot cycles and absolute temperature, finite temperature heat transfer, and ideal gas Carnot cycles. It also includes review problems at the end. The chapter examines concepts related to heat engines, refrigerators, the second law of thermodynamics, and Carnot cycles.
Engineering mechanics dynamics (6th edition) j. l. meriam, l. g. kraigeshayangreen
This document discusses the history and development of paper money. It explains that originally paper money was developed as a way to represent gold and silver coins to make large transactions more convenient. Over time, governments began to print paper money that was not backed by precious metals, which led to inflation. The document outlines some of the challenges faced by governments in managing paper currency.
This document provides thermodynamic and transport property data for several common fluids including water, steam, refrigerants, and gases. It includes tables of saturated liquid and vapor properties such as specific volume, enthalpy, and entropy. Additional tables provide properties for superheated steam, supercritical fluids, and gases at various pressures and temperatures. The document aims to serve as a reference for engineers and scientists working with these important industrial fluids.
Mechanics of materials 9th edition goodno solutions manualKim92736
This document contains solutions to problems from Chapter 2 of the 9th Edition Mechanics of Materials textbook by Goodno. It lists over 300 problems from sections 2.2 through 2.12 that have been solved, along with the full textbook reference and a link to download the full solutions manual PDF. The problems cover topics in stress, strain, Hooke's law, axial loading, torsion, shear stresses, and more.
MET 401 Chapter 6 -_gas_turbine_power_plant_brayton_cycle_-_copyIbrahim AboKhalil
This document discusses the Brayton cycle, which is the ideal gas turbine cycle. It covers:
1. The basic components and processes of the Brayton cycle, including constant pressure heat addition, isentropic expansion, and constant pressure heat rejection.
2. Key assumptions used in analyzing the cycle, such as treating air as an ideal gas and replacing combustion with heat addition.
3. Performance parameters like thermal efficiency as a function of pressure ratio and the impact of limiting turbine inlet temperatures.
4. Modifications to improve efficiency, including regeneration which recovers heat from the exhaust to preheat the compressor inlet air.
Solution manual internal combstion engine by willard w. pulkrabekDarawan Wahid
The document discusses the benefits of exercise for mental health. It states that regular exercise can help reduce anxiety and depression and improve mood and cognitive function. Exercise causes chemical changes in the brain that may help alleviate symptoms of mental illnesses.
This document repeats the same copyright statement multiple times. The statement says that excerpts from this work (a solution manual) may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation requires permission under the 1976 United States Copyright Act.
Este documento resume algunos conceptos clave en el diseño aerodinámico de planeadores. Explora cómo los diseñadores deben encontrar un equilibrio entre baja resistencia a altas velocidades y alta sustentación a bajas velocidades. También discute la importancia del número de Reynolds, la forma del ala, los perfiles aerodinámicos y el control de pérdida. El objetivo general es minimizar la resistencia y maximizar la sustentación en diferentes regímenes de vuelo.
The document discusses a website that provides free university textbooks and solutions manuals. It states that the solutions manuals contain step-by-step solutions to all the problems in the textbooks. It invites visitors to download the textbooks and solutions manuals for free.
Arizona State University Department of Physics PHY 132 –.docxjustine1simpson78276
Arizona State University
Department of Physics
PHY 132 – University Physics Lab II – Section #: 30531
TA – Alan Moran
Lab 3
Capacitors
Submitted by:
Charles Foxworthy
6 April 2015
Abstract: This lab focuses on experimenting with parallel plate capacitors. The first part of the
lab uses a test set up that allows the user to vary the surface area and the separation of plates in
a capacitor. When the plate was its smallest (100mm2) and furthest apart (10.0mm) it yielded its
lowest capacitance (0.04 pF). The first experiment demonstrated that insertion of a dielectric
increases capacitance, using a constant sized capacitor of 250mm2, with a constant separation of
7mm a dielectric was inserted and capacitance increase to 5 times its original value to 0.79pF.
Then a new dielectric was inserted and slow removed and the capacitance decreased as
expected.
Part 2 and 3 of the experiment focused on parallel and series circuits with only switches and
capacitors. The first experiment was parallel capacitors and it demonstrated that charge was
conserved and that it was additive when capacitors are parallel. Part 3 had a capacitor in
parallel with other capacitors in series. It demonstrated that charge is constant among
capacitors that are in series, and reiterated that charge is additive when capacitors are parallel.
Both experiments had an initial charge of 0.9 and that charge stayed constant throughout the
experiments.
When it was all done the theoretical values matched the experimental values and all the
experiments were successful, and the hypotheses were proven.
Objectives: 2
Procedure: ...................................................................................................................................... 3
Experimental Data: ....................................................................................................................... 15
Results: .......................................................................................................................................... 17
Discussion and Analysis: .............................................................................................................. 19
Conclusion: ................................................................................................................................... 20
1
Objective:
The purpose of this experiment is to explore capacitors. The first experiment focuses on air gap
capacitors, and exploring changes based on a bigger gap, and/or smaller plates. The second part
to that experiment adds a nonconductive material to see the effect on the capacitance. The third
part of the experiment adds a nonconductive material and slowly removes it from the capacitor
and shows its effects. The second experiment uses capacitors in parallel and charges one then
removes the power source and ch.
Intégration des énergies renouvelables dans le réseau de Grande-BretagneThearkvalais
The document discusses National Grid's work to integrate renewable energy into the UK electricity system. It outlines challenges including obtaining reserve capacity to balance the intermittent nature of renewables, utilizing surplus renewable energy to decarbonize heat and transport, and meeting peak heat demands cost effectively. Current work areas focus on system modeling, improved renewable forecasting, demand response, and engagement with stakeholders to develop solutions that ensure affordable, secure and sustainable decarbonization of the UK energy system.
This document describes a proposed algorithm to accelerate the Benders decomposition method for mixed integer programming problems. The classical Benders method cannot be directly applied when the subproblem contains integer variables. The proposed algorithm uses a branch-and-cut approach, relaxing the integer constraints and generating "local cuts" valid for descendant nodes to improve initial bounds. Computational results on capacitated knapsack and journey planning problems show the approach finds solutions over 60% faster on average than without local cuts. The algorithm allows effective use of Benders decomposition for problems where the subproblem was previously integer.
The document contains solutions to math problems using Mathcad. Section 1 covers topics including: converting between Celsius and Fahrenheit, calculating pressure, force, work, energy, and cost analysis problems. Section 2 covers additional thermodynamics problems calculating things like internal energy, enthalpy, heat transfer, and phase changes.
I am Boris M. I am a Computer Science Assignment Help Expert at programminghomeworkhelp.com. I hold an MSc. in Programming, McGill University, Canada. I have been helping students with their homework for the past 8years. I solve assignments related to Computer Science.
Visit programminghomeworkhelp.com or email support@programminghomeworkhelp.com.You can also call on +1 678 648 4277 for any assistance with Computer Science assignments.
- The document discusses using the iterative Jacobi method to solve a matrix equation representing a computational fluid dynamics (CFD) problem.
- Residuals are calculated at each iteration to measure how well the current solution satisfies the matrix equation, with residuals approaching zero indicating convergence of the solution.
- After 35 iterations, the Jacobi method solution converged to u1=1.801, u2=1.401, u3=0.4, matching the analytical solution from Excel.
This document describes the use of advanced educational technologies in a process simulation course. It discusses typical characteristics of process simulation courses, including the use of commercial simulators. It then outlines course objectives and new techniques used, such as an interface to retrieve physical property data and automatic conversion of equations to MATLAB programs. As an example, it presents the simulation of a semi-batch distillation process and results, comparing them to Aspen. It concludes that covering diverse course material requires enhancing students' programming and problem-solving skills and developing problems in line with new tool capabilities.
IRJET- Diesel Particulate Filter by using Copper Oxide as a Filter MediumIRJET Journal
This document summarizes research on using copper oxide in a diesel particulate filter to reduce carbon monoxide emissions from diesel engines. It introduces the health and environmental issues with diesel engine emissions and the need for aftertreatment devices. The study designs a particulate filter with copper oxide spheres that can react with carbon monoxide at temperatures of 400-500°C to convert it to less harmful carbon dioxide. Experimental testing of a diesel engine without and with the copper oxide filter shows reductions in carbon monoxide and other emissions with only minor reductions in engine performance.
The document summarizes updates to the 2010-2011 National Engineering Design Challenge involving building windmill devices to perform tasks. Key changes include measuring average electrical power output over time using automated equipment rather than lamps, requiring teams to measure and report the mass of their device, and extending devices over table edges and onto the floor. Teams must now submit a cost and labor summary as part of their academic display. The performance criteria for tasks raising a mass, powering a vehicle, and responding to wind direction changes remain the same.
Due to limited availability of coal and gases, optimization plays an important factor in thermal
generation problems. The economic dispatch problems are dynamic in nature as demand varies with time.
These problems are complex since they are large dimensional, involving hundreds of variables, and have
a number of constraints such as spinning reserve and group constraints. Particle Swarm Optimization
(PSO) method is used to solve these challenging optimization problems. Three test cases are studied
where PSO technique is successfully applied.
1) The document discusses using 3D mathematical models in ANSYS to improve the efficiency of aluminum reduction cells known as Hall-Héroult cells.
2) It provides an example of a company that was able to significantly reduce their power consumption and improve efficiency by retrofitting their cell design using GeniSim 3D thermo-electric models.
3) The models can simulate the thermal balance and stability of potential new cell designs through virtual prototyping before building physical prototypes to reduce costs and improve efficiency.
Subject Title: Engineering Numerical Analysis
Subject Code: ID-302
Contents of this chapter:
Mathematical preliminaries,
Solution of equations in one variable,
Interpolation and polynomial Approximation,
Numerical differentiation and integration,
Initial value problems for ordinary differential equations,
Direct methods for solving linear systems,
Iterative techniques in Matrix algebra,
Solution of non-linear equations.
Approximation theory;
Eigen values and vector;
66.-Merle C. Potter, David C. Wiggert, Bassem H. Ramadan - Mechanics of Fluid...HectorMayolNovoa
This document contains solutions to problems in a textbook on mechanics of fluids. It has 14 chapters that cover topics like fluid statics, fluids in motion, integral and differential forms of fundamental laws, dimensional analysis, internal and external flows, compressible flow, open channel flow, piping systems, and turbomachinery. Each chapter contains problems and their step-by-step solutions to aid instructors and students.
Chem 162 Lab 3: Gas Laws Part I & II- Sample Data for the class
1) Sample Data Group 1:
Part I
Part II
Volume (ml)
Pressure (kPa)
Temperature (°C)
Pressure (kPa)
103.0
60
70.8
113.5
88.0
70
66.3
112.6
73.0
85
61.8
111.5
62.0
100
57.1
110.4
44.0
140
51.5
109.0
34.0
180
39.9
105.5
31.0
200
26.4
101.8
10.5
96.7
2) Sample Data Group 2:
Part I
Part II
Volume (ml)
Pressure (Torr)
Temperature (°C)
Pressure (kPa)
32.0
630
57
109.6
29.2
690
52
108.4
27.8
726
48.5
107.4
25.6
790
43.6
106.3
24.2
843
38.1
104.8
22.2
914
33.1
103.5
29.3
102.2
25.4
101.1
22.5
100.1
20
99.4
17.4
98.6
12.8
97.2
9.4
96.7
Bellevue College | Chemistry 162
1
Empirical Gas Laws (Part 3): The Ideal Gas Law
Determination of the Universal Gas Constant, R
In this experiment, you will generate and collect a sample of hydrogen gas over water by the
reaction of magnesium with hydrochloric acid.
Using the Ideal Gas Law (PV=nRT) you will find values for the pressure (P), volume (V),
number of moles of the gas (n), and the temperature (T) in order to determine the gas constant
(R). Because there will be water vapor present in your sample, you will make a correction to the
measured pressure and then compare your result for R to the literature value.
In this experiment, you will:
Determine a value for the Universal Gas Constant, R. (Part 3 of Empirical Gas Laws)
Safety Precautions
Wear your goggles at all times. Hydrochloric acid is corrosive.
Avoid spills and contact with your skin and clothing. If HCl
comes in contact with your skin, inform your teacher and flush
the acid with large quantities of water.
Note: If you are doing Part 3 to determine the value of the Universal
Gas Constant, R in the same period as Parts 1 and 2, you should get Part 3
started first.
EXPERIMENTAL PROCEDURE (WORK IN PAIRS)
1. Put on goggles. Keep them on during the entire experiment.
2. Obtain a piece of magnesium ribbon that weighs no more than 0.08 grams. Record the mass
obtained (use significant figures!). Record this value in your data table (see report sheets).
Loosely roll it into a ball or coil it.
Encase the magnesium in a piece of copper mesh. Why do you think this might be helpful?
3. Fill the 800-mL beaker with approximately 200-mL of tap water.
4. Fill the 100-mL graduated cylinder with tap water. Using parafilm, a one-
hole stopper, or the palm of your hand, cover the top and invert the cylinder
into the beaker of water. You will end up with an inverted cylinder full of
water. Remove the parafilm or stopper if you used one. Rest the cylinder
on the bottom of the beaker. Try not to introduce any air bubbles in your
inverted cylinder (see Figure 1).
5. Place the magnesium (in its copper cage) into the graduated cylinder. Make
sure the magnesium is captured in the cylinder.
Figure 1: Gas collection in an
inverted cylinder full of water.
This document provides a summary of a research project on modeling the degradation of solar photovoltaic modules over time. It examines modules installed at two solar power plants in India - a 1 MW plant on an ash dyke and a 1 MW canal top plant. Testing showed canal top modules had lower temperatures and higher performance. The project developed loss models and found polycrystalline modules degraded 1.73-3.89% annually at one plant and 0.17-1.95% at the other. Regular cleaning can avoid a 1.61% efficiency loss from soiling. The models matched simulated results within a few percent.
Shortcut Design Method for Multistage Binary Distillation via MS-ExceIJERA Editor
Multistage distillation is most widely used industrial method for separating chemical mixtures with high energy consumptions especially when relative volatility of key components is lower than 1.5. The McCabe Thiele is considered to be the simplest and perhaps most instructive method for the conceptual design of binary distillation column which is still widely used, mainly for quick preliminary calculations. In this present work, we provide a numerical solution to a McCabe-Thiele method to find out theoretical number of stages for ideal and non-ideal binary system, reflux ratio, condenser duty, reboiler duty, each plate composition inside the column. Each and every point related to McCabe-Thiele in MS-Excel to give quick column dimensions are discussed in details
This document describes a simplified SPICE behavioral model for a maximum peak power tracker (MPPT) and DC/DC converter combination. The model focuses on the input/output relationships rather than circuit details, allowing long-term system simulation over 100 times faster than a cycle-to-cycle model. It is characterized by parameters like efficiency, input/output voltages, and current sensing that represent the converter's behavior. Transient simulations demonstrate how the MPPT tracks the solar cells' maximum power point under changing light intensity conditions.
text book Programmable-Logic-Controllers plc.pdfMahamad Jawhar
This document provides an overview and introduction to programmable logic controllers (PLCs). It discusses the basic parts and components of a PLC including the input/output section, central processing unit, memory, and programming devices. It also describes the basic principles of how PLCs operate by scanning inputs, executing a user-created program, and updating outputs. The document is intended to familiarize readers with the basic concepts and components of PLCs.
Kurdistan Regional Government Iraq Ministry of Electricity generates electricity primarily from fossil fuels such as natural gas. Renewable energy sources such as hydro, solar, wind, and geothermal currently account for a smaller portion of electricity generation but their use is growing. Geothermal energy harnesses heat from within the earth through technologies such as hydrothermal, geopressure, and hot dry rock systems to generate electricity without directly burning fuels. Geothermal resources in the Kurdistan region show potential for development to increase renewable energy supply and reduce dependence on fossil fuels.
This document appears to be a resume for Zeyad Azeez Abdullah, a mechanical engineer. It includes his name, title, date, and sections on qualifications, experience, education, skills and interests. There are also diagrams and specifications for solar panels, batteries, and other energy related topics.
Muhammad Jawhar Anwar built a helicopter robot for his Fourth Stage A1 class at Salahaddin University-Erbil's Mechanical & Mechatronics department. The robot uses a DC motor to rotate its rotor and has an LED light, buzzer, and logic programming to move straight, rotate clockwise and counterclockwise, turn the orange LED on while moving backward, and turn the green LED on.
Power Plant Engineering - (Malestrom) (1).pdfMahamad Jawhar
This document is the preface to a book on power plant engineering. It discusses the motivation for writing the book, which was to benefit students and researchers by covering key topics in power generation in a clear and concise manner. The preface notes that the book aims to satisfy engineering scholars and researchers by addressing conventional power plant topics at an international level. It also acknowledges those who encouraged and supported the authors in writing this pioneering textbook.
This document provides an index and specifications for various optical measuring instruments, including profile projectors and microscopes. It lists several models of profile projectors from the PJ-A3000 and PJ-H30 series, along with their specifications, optional accessories, and available fixtures. It also lists several models of measuring microscopes from the MF, MF-U, and MSM-400 series, along with their specifications and optional accessories. The document provides detailed information on the specifications, features, and options for these optical measuring instruments.
This document discusses refrigeration and its various applications and methods. It begins by defining refrigeration as the process of achieving and maintaining a temperature below surroundings through the removal of heat. The main types of refrigeration are then listed as domestic, commercial, industrial, marine, air conditioning, and food preservation. Various natural and early mechanical refrigeration techniques are described, such as the use of icehouses and evaporative cooling. The ideal vapor compression refrigeration cycle is explained through its four processes. Absorption refrigeration using ammonia-water and lithium bromide-water systems is also summarized. Compressor types including reciprocating, rotary, and centrifugal are defined. Key refrigeration system components and their functions are outlined.
This document provides an introduction to programmable logic controllers (PLCs). It defines a PLC as a specialized computer that monitors processes and controls machinery. The document outlines the history of PLCs in automating factory processes. It also describes the components of a basic PLC system and lists advantages such as flexibility, ease of programming, and reliability compared to traditional relay-based controls.
This document discusses the design of a CNC plasma cutting machine. It begins with an introduction to plasma cutting, explaining that plasma cutting uses a high-temperature jet of plasma gas to cut electrically conductive materials like metals. It then provides a flow chart showing the basic components and process of a plasma cutter. The document goes on to discuss the technical details of designing a CNC plasma cutting machine, including the mechanical components, electrical systems, and software setup required to automate the plasma cutting process through computer numerical control.
This document appears to be a research project report from Salahaddin University's College of Engineering for the 2018-2019 year. The report was prepared by 4 students and supervised by a faculty member. It includes sections on the introduction, methodology, conclusion, references, and images or figures related to the research project.
This document appears to be a template for a student project submitted to the Mechanical Engineering Department at Salahaddin University-Erbil in Iraq. The template provides an outline for the typical sections included in an engineering student project paper, such as an abstract, acknowledgements, table of contents, references, etc. It also includes placeholders for the student to include the introduction, methodology, example analysis and design, results and discussion, and conclusion sections. The introduction section provides background on the project and defines the problem statement, objectives and outline. The methodology section details the analysis procedures. The example section applies the methodology to a relevant problem. The results, discussion and conclusion sections present and interpret the findings and link them back to the
The document describes a PLC program for controlling a water filling and discharging process in a tank. The program uses two level sensors, one for high level and one for low level, to control a feeding valve and discharge valve. When the low level sensor is triggered, the feeding valve turns on to fill the tank, and when the high level sensor is triggered, the discharge valve turns on to empty the tank. The program is designed to maintain the water level between the two sensor points.
This document summarizes a student project to control a two-directional traffic light using a PLC. It introduces the use of traffic lights to control vehicle and pedestrian traffic. Timers are used to provide time delays to control the light sequences. A ladder logic diagram is programmed with contacts that simulate relays to control the red and green lights for each of the three poles in sequences, with one pole green at a time for a set period before moving to the next pole. The process then repeats continuously to control traffic flow in both directions.
This document summarizes different types of cooling towers. It describes how cooling towers work by bringing air and water into contact to reduce the water's temperature through evaporation. It discusses the components of cooling towers, including fill materials, drift eliminators, nozzles, fans, and driveshafts. It also compares crossflow and counterflow cooling towers and how they differ in their water and air flow configurations. Finally, it outlines the differences between factory-assembled and field-erected cooling towers.
This document is a research project submitted in partial fulfillment of the requirements for a degree in Mechanical and Mechatronics Engineering. It contains an abstract, introduction, and 4 chapters that discuss cooling towers, their components, thermal performance testing, and electrical components. The introduction provides background on cooling towers and how they work to lower water temperature through evaporation and heat transfer to the atmosphere. It also discusses prior research on improving cooling tower performance. The abstract indicates the research examines different types of cooling towers, their application, efficiency, and working principles, and includes a simulation of flow fields around a cooling tower.
This document is a research project submitted for a degree in Mechanical and Mechatronics Engineering on cooling towers. It includes 4 chapters that discuss mechanical components, thermal performance testing, and electrical components of cooling towers. The introduction provides background on cooling towers and how they work to remove heat from water through evaporation. It also discusses types of cooling towers, including natural draft and mechanical draft, and covers psychrometrics and heat transfer principles.
1. The document compares three types of cooling towers - wet, dry, and hybrid - that are used in closed cooling systems for large power reactors.
2. It outlines the procedures for dimensioning each type of cooling tower, including calculating heat and mass transfer, air and water flows, electric power needs, and water loss. Equations used for each type are presented.
3. Results from dimensioning a 100 MW cooling tower of each type for a highland region in Algeria are presented to compare electricity consumption and water loss between the three options.
The document is a homework assignment submitted by Ahmed Naseh Latif, a student in the 4th stage of the Mechanic and Mechatronic Engineering department at Salahaddin University-Erbil. The assignment asks the student to list 10 applications of robots in real life with pictures. The student provides 10 applications: 1) automated transportation, 2) security/defense/surveillance, 3) robot cooking, 4) medicine, 5) education, 6) home maintenance, 7) dangerous jobs, 8) as a servant, 9) as a friend, and 10) crime fighting. The student includes references from books and articles on the history and uses of robotics.
Brian Peck Leonardo DiCaprio: A Unique Intersection of Lives and Legaciesgreendigital
Introduction
The world of Hollywood is vast and interconnected. filled with countless stories of collaboration, friendship, and influence. Among these tales are the notable narratives of Brian Peck and Leonardo DiCaprio. The keyword "Brian Peck Leonardo DiCaprio" might not immediately ring a bell for everyone. but the connection between these two figures in the entertainment industry is intriguing and significant. This article delves deep into their lives, careers, and the moments where their paths intersect. providing a comprehensive look at how their stories intertwine.
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Early Life and Career Beginnings
Brian Peck: The Early Years
Brian Peck was born in New York City on July 29, 1960. From a young age, Peck exhibited a passion for the performing arts. He attended the Professional Children's School. which has a history of nurturing young talent in the arts. Peck's early career marked by a series of roles in television and film that showcased his versatility as an actor.
Peck's breakthrough came with his role in the cult classic "The Return of the Living Dead" (1985). His performance as Scuz, one of the punk rockers who releases a toxic gas that reanimates the dead. earned him a place in the annals of horror cinema. This role opened doors for Peck. allowing him to explore various facets of the entertainment industry. including writing and directing.
Leonardo DiCaprio: From Child Star to Hollywood Icon
Leonardo DiCaprio was born in Los Angeles, California, on November 11, 1974. His career began at a young age with appearances in television commercials and educational films. DiCaprio's big break came when he joined the cast of the popular sitcom "Growing Pains" (1985-1992). where he played the character Luke Brower.
DiCaprio's transition from television to film was seamless. He gained recognition for his role in "This Boy's Life" (1993) alongside Robert De Niro. This performance began a series of acclaimed roles. establishing DiCaprio as one of the most talented actors of his generation. His portrayal of Jack Dawson in James Cameron's "Titanic" (1997) catapulted him to global stardom. solidifying his status as a Hollywood icon.
Brian Peck Leonardo DiCaprio: Their Paths Cross
Collaborations and Connections
The keyword "Brian Peck Leonardo DiCaprio" signifies more than two names; it represents a fascinating connection in Hollywood. While their careers took different trajectories, their paths crossed in the 1990s. Brian Peck worked with DiCaprio on the set of the 1990s sitcom "Growing Pains." where DiCaprio had a recurring role. Peck appeared in a few episodes. contributing to the comedic and dynamic environment of the show.
Their professional relationship extended beyond "Growing Pains." Peck directed DiCaprio in several educational videos for the "Disneyland Fun" series. where DiCaprio's youthful charm and energy were evident. These early collaborations offered DiCaprio valuable experience in front of the camera. he
The Future of Independent Filmmaking Trends and Job OpportunitiesLetsFAME
The landscape of independent filmmaking is evolving at an unprecedented pace. Technological advancements, changing consumer preferences, and new distribution models are reshaping the industry, creating new opportunities and challenges for filmmakers and film industry jobs. This article explores the future of independent filmmaking, highlighting key trends and emerging job opportunities.
Tom Cruise Daughter: An Insight into the Life of Suri Cruisegreendigital
Tom Cruise is a name that resonates with global audiences for his iconic roles in blockbuster films and his dynamic presence in Hollywood. But, beyond his illustrious career, Tom Cruise's personal life. especially his relationship with his daughter has been a subject of public fascination and media scrutiny. This article delves deep into the life of Tom Cruise daughter, Suri Cruise. Exploring her upbringing, the influence of her parents, and her current life.
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Introduction: The Fame Surrounding Tom Cruise Daughter
Suri Cruise, the daughter of Tom Cruise and Katie Holmes, has been in the public eye since her birth on April 18, 2006. Thanks to the media's relentless coverage, the world watched her grow up. As the daughter of one of Hollywood's most renowned actors. Suri has had a unique upbringing marked by privilege and scrutiny. This article aims to provide a comprehensive overview of Suri Cruise's life. Her relationship with her parents, and her journey so far.
Early Life of Tom Cruise Daughter
Birth and Immediate Fame
Suri Cruise was born in Santa Monica, California. and from the moment she came into the world, she was thrust into the limelight. Her parents, Tom Cruise and Katie Holmes. Were one of Hollywood's most talked-about couples at the time. The birth of their daughter was a anticipated event. and Suri's first public appearance in Vanity Fair magazine set the tone for her life in the public eye.
The Impact of Celebrity Parents
Having celebrity parents like Tom Cruise and Katie Holmes comes with its own set of challenges and privileges. Suri Cruise's early life marked by a whirlwind of media attention. paparazzi, and public interest. Despite the constant spotlight. Her parents tried to provide her with an upbringing that was as normal as possible.
The Influence of Tom Cruise and Katie Holmes
Tom Cruise's Parenting Style
Tom Cruise known for his dedication and passion in both his professional and personal life. As a father, Cruise has described as loving and protective. His involvement in the Church of Scientology, but, has been a point of contention and has influenced his relationship with Suri. Cruise's commitment to Scientology has reported to be a significant factor in his and Holmes' divorce and his limited public interactions with Suri.
Katie Holmes' Role in Suri's Life
Katie Holmes has been Suri's primary caregiver since her separation from Tom Cruise in 2012. Holmes has provided a stable and grounded environment for her daughter. She moved to New York City with Suri to start a new chapter in their lives away from the intense scrutiny of Hollywood.
Suri Cruise: Growing Up in the Spotlight
Media Attention and Public Interest
From stylish outfits to everyday activities. Suri Cruise has been a favorite subject for tabloids and entertainment news. The constant media attention has shaped her childhood. Despite this, Suri has managed to maintain a level of normalcy, thanks to her mother's efforts.
The Evolution and Impact of Tom Cruise Long Hairgreendigital
Tom Cruise is one of Hollywood's most iconic figures, known for his versatility, charisma, and dedication to his craft. Over the decades, his appearance has been almost as dynamic as his filmography, with one aspect often drawing significant attention: his hair. In particular, Tom Cruise long hair has become a defining feature in various phases of his career. symbolizing different roles and adding layers to his on-screen characters. This article delves into the evolution of Tom Cruise long hair, its impact on his roles. and its influence on popular culture.
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Introduction
Tom Cruise long hair has often been more than a style choice. it has been a significant element of his persona both on and off the screen. From the tousled locks of the rebellious Maverick in "Top Gun" to the sleek, sophisticated mane in "Mission: Impossible II." Cruise's hair has played a pivotal role in shaping his image and the characters he portrays. This article explores the various stages of Tom Cruise long hair. Examining how this iconic look has evolved and influenced his career and broader fashion trends.
Early Days: The Emergence of a Style Icon
The 1980s: The Birth of a Star
In the early stages of his career during the 1980s, Tom Cruise sported a range of hairstyles. but in "Top Gun" (1986), his hair began to gain significant attention. Though not long by later standards, his hair in this film was longer than the military crew cuts associated with fighter pilots. adding a rebellious edge to his character, Pete "Maverick" Mitchell.
Risky Business: The Transition Begins
In "Risky Business" (1983). Tom Cruise's hair was short but longer than the clean-cut styles dominant at the time. This look complemented his role as a high school student stepping into adulthood. embodying a sense of youthful freedom and experimentation. It was a precursor to the more dramatic hair transformations in his career.
The 1990s: Experimentation and Iconic Roles
Far and Away: Embracing Length
One of the first films in which Tom Cruise embraced long hair was "Far and Away" (1992). Playing the role of Joseph. an Irish immigrant in 1890s America, Cruise's long, hair added authenticity to his character's rugged and determined persona. This look was a stark departure from his earlier. more polished styles and marked the beginning of a more adventurous phase in his hairstyle choices.
Interview with the Vampire: Gothic Elegance
In "Interview with the Vampire" (1994). Tom Cruise long hair reached new lengths of sophistication and elegance. Portraying the vampire Lestat. Cruise's flowing blonde locks were integral to the character's ethereal and timeless allure. This hairstyle not only suited the gothic aesthetic of the film but also showcased Cruise's ability to transform his appearance for a role.
Mission: Impossible II: The Pinnacle of Long Hair
One of the most memorable instances of Tom Cruise long hair came in "Mission: Impossible II" (2000). His character, Ethan
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At 28, Brianna Coppage left her teaching career to become an OnlyFans content creator. This bold move into digital entrepreneurship allowed her to harness her creativity and build a new identity. Brianna's experience highlights the intersection of technology and personal branding in today's economy.
Taylor Swift: Conquering Fame, Feuds, and Unmatched Success | CIO Women MagazineCIOWomenMagazine
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Leonardo DiCaprio House: A Journey Through His Extravagant Real Estate Portfoliogreendigital
Introduction
Leonardo DiCaprio, A name synonymous with Hollywood excellence. is not only known for his stellar acting career but also for his impressive real estate investments. The "Leonardo DiCaprio house" is a topic that piques the interest of many. as the Oscar-winning actor has amassed a diverse portfolio of luxurious properties. DiCaprio's homes reflect his varied tastes and commitment to sustainability. from retreats to historic mansions. This article will delve into the fascinating world of Leonardo DiCaprio's real estate. Exploring the details of his most notable residences. and the unique aspects that make them stand out.
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Leonardo DiCaprio House: Malibu Beachfront Retreat
A Prime Location
His Malibu beachfront house is one of the most famous properties in Leonardo DiCaprio's real estate portfolio. Situated in the exclusive Carbon Beach. also known as "Billionaire's Beach," this property boasts stunning ocean views and private beach access. The "Leonardo DiCaprio house" in Malibu is a testament to the actor's love for the sea and his penchant for luxurious living.
Architectural Highlights
The Malibu house features a modern design with clean lines, large windows. and open spaces blending indoor and outdoor living. The expansive deck and patio areas provide ample space for entertaining guests or enjoying a quiet sunset. The house has state-of-the-art amenities. including a gourmet kitchen, a home theatre, and many guest suites.
Sustainable Features
Leonardo DiCaprio is a well-known environmental activist. whose Malibu house reflects his commitment to sustainability. The property incorporates solar panels, energy-efficient appliances, and sustainable building materials. The landscaping around the house is also designed to be water-efficient. featuring drought-resistant plants and intelligent irrigation systems.
Leonardo DiCaprio House: Hollywood Hills Hideaway
Privacy and Seclusion
Another remarkable property in Leonardo DiCaprio's collection is his Hollywood Hills house. This secluded retreat offers privacy and tranquility. making it an ideal escape from the hustle and bustle of Los Angeles. The "Leonardo DiCaprio house" in Hollywood Hills nestled among lush greenery. and offers panoramic views of the city and surrounding landscapes.
Design and Amenities
The Hollywood Hills house is a mid-century modern gem characterized by its sleek design and floor-to-ceiling windows. The open-concept living space is perfect for entertaining. while the cozy bedrooms provide a comfortable retreat. The property also features a swimming pool, and outdoor dining area. and a spacious deck that overlooks the cityscape.
Environmental Initiatives
The Hollywood Hills house incorporates several green features that are in line with DiCaprio's environmental values. The home has solar panels, energy-efficient lighting, and a rainwater harvesting system. Additionally, the landscaping designed to support local wildlife and promote
Morgan Freeman is Jimi Hendrix: Unveiling the Intriguing Hypothesisgreendigital
In celebrity mysteries and urban legends. Few narratives capture the imagination as the hypothesis that Morgan Freeman is Jimi Hendrix. This fascinating theory posits that the iconic actor and the legendary guitarist are, in fact, the same person. While this might seem like a far-fetched notion at first glance. a deeper exploration reveals a rich tapestry of coincidences, speculative connections. and a surprising alignment of life events fueling this captivating hypothesis.
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Introduction to the Hypothesis: Morgan Freeman is Jimi Hendrix
The idea that Morgan Freeman is Jimi Hendrix stems from a mix of historical anomalies, physical resemblances. and a penchant for myth-making that surrounds celebrities. While Jimi Hendrix's official death in 1970 is well-documented. some theorists suggest that Hendrix did not die but instead reinvented himself as Morgan Freeman. a man who would become one of Hollywood's most revered actors. This article aims to delve into the various aspects of this hypothesis. examining its origins, the supporting arguments. and the cultural impact of such a theory.
The Genesis of the Theory
Early Life Parallels
The hypothesis that Morgan Freeman is Jimi Hendrix begins by comparing their early lives. Jimi Hendrix, born Johnny Allen Hendrix in Seattle, Washington, on November 27, 1942. and Morgan Freeman, born on June 1, 1937, in Memphis, Tennessee, have lived very different lives. But, proponents of the theory suggest that the five-year age difference is negligible and point to Freeman's late start in his acting career as evidence of a life lived before under a different identity.
The Disappearance and Reappearance
Jimi Hendrix's death in 1970 at the age of 27 is a well-documented event. But, theorists argue that Hendrix's death staged. and he reemerged as Morgan Freeman. They highlight Freeman's rise to prominence in the early 1970s. coinciding with Hendrix's supposed death. Freeman's first significant acting role came in 1971 on the children's television show "The Electric Company," a mere year after Hendrix's passing.
Physical Resemblances
Facial Structure and Features
One of the most compelling arguments for the hypothesis that Morgan Freeman is Jimi Hendrix lies in the physical resemblance between the two men. Analyzing photographs, proponents point out similarities in facial structure. particularly the cheekbones and jawline. Both men have a distinctive gap between their front teeth. which is rare and often highlighted as a critical point of similarity.
Voice and Mannerisms
Supporters of the theory also draw attention to the similarities in their voices. Jimi Hendrix known for his smooth, distinctive speaking voice. which, according to some, resembles Morgan Freeman's iconic, deep, and soothing voice. Additionally, both men share certain mannerisms. such as their calm demeanor and eloquent speech patterns.
Artistic Parallels
Musical and Acting Talents
Jimi Hendrix was regarded as one of t
Abraham Laboriel Records ‘The Bass Walk’ at Evergreen Stage
AC 6Ed.pdf
1. SOLUTIONS MANUAL
Heating, Ventilating and Air Conditioning
Analysis and Design
Sixth Edition
Faye C. McQuiston
Jerald D. Parker
Jeffrey D. Spitler
John Wiley & Sons
2004
M16FMR
m16fmr@hotmail.co.uk
USE IT WITH YOUR MIND
M
1
6
F
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2. PREFACE
This manual consists of solutions for the text problems, Chapters 1
through 15. Many of the problems with a design orientation have more
than one acceptable solution. Therefore, when an acceptable solution
may be quite variable or closely follows an example, the solution may be
omitted or only general guidelines given.
The degree of difficulty and length of the problems vary
considerably. In many cases the problem statement should be discussed
in class prior to assignment. This manual should be helpful in this
respect.
The use of computer software is strongly encouraged. Many
problems can be solved by hand or computer calculations. Most of these
problems are in Chapters 3, 7, 8, 10, 12 and 14. A number of problems
are designed for solution using the software distributed with the website.
A great effort has been made to eliminate errors in the solutions;
however, some probably still exist. Please see the addendum to this
manual for assumptions used in problems 6-10, 7-9, 7-14, 8-25, and 8-26.
The authors would appreciate notification of any errors discovered.
Faye C. McQuiston
Jerald D. Parker
Jeffrey D. Spitler
M16FMR
m16fmr@hotmail.co.uk
USE IT WITH YOUR MIND
M
1
6
F
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4. CONTENTS
Chapter 1 Introduction 1-6
Chapter 2 Air-Conditioning Systems 7
Chapter 3 Moist Air Properties and Conditioning 8-65
Processes
Chapter 4 Comfort and Health – Indoor Environmental 66-78
Quality
Chapter 5 Heat Transmission in Building Structures 79-92
Chapter 6 Space Heat Load 93-105
Chapter 7 Solar Radiation 106-129
Chapter 8 The Cooling Load 130-183
Chapter 9 Energy Calculations and Building Simulation 184-188
Chapter 10 Flow, Pumps, and Piping Design 189-210
Chapter 11 Space Air Diffusion 211-219
Chapter 12 Fans and Building Air Distribution 220-259
Chapter 13 Direct Contact Heat and Mass Transfer 260-265
Chapter 14 Extended Surface Heat Exchangers 266-298
Chapter 15 Refrigeration 299-310
Addendum 311-312
M16FMR
m16fmr@hotmail.co.uk
USE IT WITH YOUR MIND
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5. Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for
testing or instructional purposes only to students enrolled in courses for which the textbook has been
adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or
108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
Requests for permission or further information should be addressed to the Permission Department,
John Wiley & Sons, Inc, 111 River Street, Hoboken, NJ 07030.
PREFACE
This manual consists of solutions for the text problems, Chapters 1
through 15. Many of the problems with a design orientation have more
than one acceptable solution. Therefore, when an acceptable solution
may be quite variable or closely follows an example, the solution may be
omitted or only general guidelines given.
The degree of difficulty and length of the problems vary
considerably. In many cases the problem statement should be discussed
in class prior to assignment. This manual should be helpful in this
respect.
The use of computer software is strongly encouraged. Many
problems can be solved by hand or computer calculations. Most of these
problems are in Chapters 3, 7, 8, 10, 12 and 14. A number of problems
are designed for solution using the software distributed with the website.
A great effort has been made to eliminate errors in the solutions;
however, some probably still exist. Please see the addendum to this
M16FMR
m16fmr@hotmail.co.uk
USE IT WITH YOUR MIND
M
1
6
F
M
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6. Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes
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beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner
is unlawful.
manual for assumptions used in problems 6-10, 7-9, 7-14, 8-25, and 8-26.
The authors would appreciate notification of any errors discovered.
Faye C. McQuiston
Jerald D. Parker
Jeffrey D. Spitler
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7. 311
ADDENDUM
to
Solutions Manual for McQuiston, HVAC 6e
Problem 6-10
For the floor, it is unclear what 2 in. vertical edge insulation means (whether 2 in. is the
thickness of insulation or the depth of the edge insulated).
• The solution assumes that the insulation has R-value of 5.4 hr-ft²-°F/Btu and the
depth of the edge is 2 ft.
For the door, Table 5-8 in the 6th
edition does not have U-value for the wood storm door
and there are three types of the wood door with 1 ¾ in. thickness.
• The solution assumes that the doors are panel doors with metal storm door; hence,
its U-value is 0.28 But/hr-ft²-°F.
Problem 7-9
The standard time zone for Ottawa, Ontario is Eastern Standard Time instead of Central
Standard Time.
• The solution uses Eastern Standard Time.
Problem 7-14
For the specified location, the sunset occurs before 9:00 p.m. CDST on June 21.
• The solution uses 8:00 p.m. CDST instead of 9:00 p.m.
Problems 8-25 and 8-26
Both problems do not specify the window orientation.
• The solutions assume the west-facing window for both problems.
Table 8-20
Recommended radiative and convective fractions for solar heat gains should be revised
since the 6th
edition uses the SHGC values in the calculation of the (combined) solar heat
gain for the RTS method.
Example 8-16
The example actually uses 90%/10% of radiative/convective split of the combined solar
heat gain. However, the text (page 270) says 100%/0% for the transmitted solar heat gain
and 63%/37% for the absorbed solar heat gain.
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8. 312
Problems 8-25 and 8-26
The solutions for both problems use 90%/10% for the combined solar heat gain.
Example 9-1
The calculation for this example should be
606
,
122
)
1000
)(
0
70
)(
55
.
0
(
)
66
.
0
)(
000
,
80
)(
3725
)(
24
(
=
−
=
F .
(Changing 13 to 24 and 122790 to 122606).
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testing or instructional purposes only to students enrolled in courses for which the textbook has been
adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108
of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
Requests for permission or further information should be addressed to the Permission Department, John
Wiley & Sons, Inc, 111 River Street, Hoboken, NJ 07030.
Chapter 1
1-1 (a) 98 Btu/(hr-ft-F) x1.7307 = 170 W/(m-K)
(b) 0.24 Btu/(Ibm-F) x4186.8=1.0 kJ/kg-K
(c)
0.04 Ibm/(ft-hr)
3600 sec/hr
x1.488 = 16.5 2
Ns
m
µ
(d) 1050
Btu
Ibm
x 4
1
9.48x10−
J
Btu
x
2.20462 Ibm
kg
= 2.44
MJ
kg
(e) 12,000
Btu
Ibm
x
1
3.412
= 3.52 kW
(f) 14.7 2
Ibf
in
x 6894.76 = 101 kPa
1-2 (a) 120 kPa x
2
lbf /in
6.89476kPa
= 17.4 lbf/in2
(b) 100
W
m K
−
x 0.5778 = 57.8 Btu/hr-ft-F
(c) 0.8 2
W
m K
−
x 0.1761 = 0.14 Btu/hr-ft2
-F
(d) 10-6
N-s/m2
x
1
1.488
= 6.7 x 10-7 lbm
ft sec
−
(e) 1200 kW x 3412 = 4.1 x 10-6
Btu/hr
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10. 2
(f) 1000
kJ
kg
x
1 Btu
1.055 kJ
x
1 kg
2.2046 lbm
= 430
Btu
lbm
1-3 Hp = 50 (ft) x 0.3048 (
m
ft
) = 15.2 m
∆ P =
15.2 m
1000 Pa/kPa
x
9.807
1
(
N
kg
) x 1000 (kg/m3
) = 149 kPa
1-4 P =
∆
4
12
(ft) x 0.3048 (
m
ft
) x
9.807
1
(
N
kg
) x 1000 ( 3
kg
m
)
∆ P = 996 Pa 1.0 kPa
≈
1-5
TOTAL BILL = ENERGY CHARGE + DEMAND CHARGE
+ METER CHARGE
( ) ( ) ( ) ( )
96,000 kw - hrs 0.045 $/kw hr + 624 kw 11 50 $/kw
− −
+ $68 = $4,320 + $7,176 + $68 = $11,564
1-6 7 AM to 6 PM 11 hrs/day, 5 days/wk
hrs days
(11) (22) 242 hrs/month
day months
=
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11. 3
( )
( )
( )
624 kw
ratio = 1.57
96,000 kw hr
242 hr
=
⎛ ⎞
−
⎜ ⎟
⎝ ⎠
1-7 This is a trial and error solution since eq. 1-1 cannot be solved
explicitly for i.
Answer converges at just over 4.2% using eq. 1-1
1-8 Determine present worth of savings using eq. 1-1
( )
( )( )
12 12
0.012
$1000 1- 1+
12
P =
0.012
12
P $134,000
−
⎡ ⎤
⎛ ⎞
⎢ ⎥
⎜ ⎟
⎝ ⎠
⎢ ⎥
⎣ ⎦
⎛ ⎞
⎜ ⎟
⎝ ⎠
=
1-9 (a) Q VA
=
= 2 x 3.08 x 10-3
= 6.16 x 10-3
m3
/s
m 6.16 x 10
Q
ρ
=
= -3
x 998 = 6.15 kg/s
(b) A=
4
π
(0.3)2
= 7.07 x 10-2
m2
Q 7.07x10
=
-2
x 4 = 0.283 m3
/ s; ρ = 1.255 kq/m3
m = 1.225 x 0.283 = 0.347 kg/s
1-10 V = 3x10x20 = 600m3
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12. 4
= 600 x
i
Q
1
4
x
1
3600
= 4.17 x 10-2
m3
/s
1-11
p p
3
q = mc T c = 4.183 kJ/(kg-K)
= 983.2 kg/m
ρ
∆
1-11 (cont’d)
( ) ( ) ( ) ( )
3
c
3
m kg kJ
q = 1 983.2 4.183 5 20,564
s kg K
m
q = 20,564 kw
=
−
kJ
s
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1-12 =
wat
q
air
q
−
11,200(1)(10) =
= 2
5000x60x14.7x144x0.24(t 50)
(53.35x510)
−
11,200 = 5601.5 (t2-50); t2 = (11,200/5601.5) + 50 = 70 F
1-13 Diagram as in 1-12 above.
q
wat = -q
air
1.5 (4186)(90-t2) = 2.4 (1.225)(1.0)(30-20)(1000)
6279(90-t2) = 29,400
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students enrolled in courses for which the textbook has been adopted. this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permissi
5
t2 = 90 -
29,400
6279
= 85.3 C
1-14 q hA(t
=
s- )
t∞
A= π (1/12) x 10 = 2.618 ft2
s
t = tsur 212 F
≈
= 10x2.618x(212-50) = 4241 Btu/hr
q
1-15 A= π x 0.25x4 = 3.14 16 m2
hA(t
q =
s- )
t∞
h=
s
q
A(t -t )
∞
=
1250
3.1416(100 10)
−
; h = 4.42 W/(m2
– C)
1-16 (t
p
q mc
=
2-t1) ; m Q x ρ
=
ρ = P/RT = 14.7x144/53.35(76+460)
ρ = 0.074 lbm/ft3
m = 5000x0.074x60 = 22,208 lbm/hr
= 0.24 Btu/lbm-F
p
c
q= 22,208x0.24(58-76) = -95,939 Btu/hr
Negative sign indicates cooling
1-17 (t
1 p
m c
3-t1) +
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14. 6
(t
2 p2
m c
3-t2) = 0
=
p1
c p2
c
t3 = 1 1 2 2
1 2
(m t m t )
(m m )
+
+
1 2
m Q 1
ρ
=
= 1000x
14.7x144
53.35(460 50)
+
= 73.5 lbm/min
1-17 (cont’d)
2 2
m Q 2
ρ
=
= 600x
14.7x144
53.35(460 50)
+
= 46.7 lbm/min
3
(73.5x80) (46.7 x 50)
t 68.3 F
(73.5 46.7)
+
= =
+
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15. 7
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Wiley Sons, Inc, 111 River Street, Hoboken, NJ 07030.
Chapter 2
2-1 through 2-20
Solutions are not furnished since many acceptable responses exist
for each problem. It is not expected that the beginning student can handle
these questions easily. The objective is to make the student think about
the complete design problem and the various functions of the system.
These problems are also intended for use in class discussions to enlarge
the text material.
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testing or instructional purposes only to students enrolled in courses for which the textbook has been
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Wiley Sons, Inc, 111 River Street, Hoboken, NJ 07030.
Chapter 3
3-1 (a) Pv = =
s
rP
φ 0.45(3.17)kPa = 1.43 kPa or 0.45(0.435) = 0.196 psia
Pa = 101 – 1.43 = 99.57 kPa or 14.696-0.196 = 14.5 psia
(b) =
v
v
P
ρ
RvT or = = = 3
v
v v
v
P 1430
ρ ; ρ 0.0104 kg/m
R T 462.5(297)
or =
0.196(144)
0.00062
85.78(535)
lbv/ft3
(c) W =
0.6219 (1.43)
(99.57)
= 0.00893 kgv/kga
or
0.6219(0.196)
0.00854 lbv/lba
14.5
=
3-2 (a) English Units – t = 80F; P = 14.696 psia;
Pv = 0.507 psia Table A-1a
W = 0.6219
a
v
P
P
=
0.6219 (0.507)
(14.696 0.507)
−
= 0.0222 lbv/lba
i = 0.24t + W(1062.2 + 0.444t)
i = 0.24 (80) + 0.0222[1061.2 + 0.444(80)] = 43.55 Btu/lbm
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17. 8
v =
a
a
R T 53.35(460 80)
P (14.696 0.507)144
+
=
−
= 13.61 ft3
/lbm
(b) English Units – 32F, 14.696 psia
Pv = 0.089 psia (Table A-1)
3-2 (cont’d)
W =
0.6219(0.089) lbmv
0.00379
(14.696 0.089) lbma
=
−
i = 0.24(32) + 0.00379 [1061.2 + 0.444(32)] = 11.76 Btu/lbma
v =
53.35(492)
(14.696 0.089)144
−
= 12.48 ft3
/lbma
3-2 (a) SI Units – 27C; 101.325 kPa
Pv = 3.60 kPa, Table A-1b
W = 0.6219 v
a
P 0.6219(3.6) kgv
0.0229
P (101.325 3.6) kga
= =
−
i = 1.0t + W(2501.3 + 1.86t) kJ/kga
i = 27 + 0.0229(2501.3 + 1.86 x 27) = 85.43 kJ / kga
v = 3
a
a
R T 0.287(300)
= =0.88 m /kga
P (101.325 - 3.6)
(b) SI Units 0.0C; 101.325 kPa
Pv = 0.61 kPa, Table A-1b
W =
0.6219(0.61)
=0.00377 kgv/kga
(101.325 - 0.61)
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18. 9
i = 0.0 + 0.00377 (2501.3 – 1.86 x 0.0) = 9.42 kJ/kga
v =
3
0.287(273)
0.778 m /kga
(101.325 - 0.61)
=
3-3 (a) English Units – 5000 ft elevation, P = 12.24 psia = 24.92 in.Hg
t = 80 F; Pv = 0.507 psia (Table A-1a)
W = 0.6219
v
a
P 0.6219(0.507)
=
P (12.24 - 0.507)
= 0.0269 lbv/lba
i = 0.24(80) + 0.0269 [1061.2 + 0.444(80)] = 48.7 Btu/lbma
v = a
a
R T 53.35(540)
=
P (12.24 - 0.507) 144
= 17.05 ft3
/ lbma
(b) English Units – t = 32 F, Pv = 0.089 psia ( Table A-1a)
W =
0.6219(0.089)
(12.24 0.089)
−
= 0.00456 lbmv/lbma
i = 0.24(32) + 0.00456 [1061.2 + 0.444(32)] =12.58 Btu/lbma
v =
53.35(492)
(12.24 0.089)144
−
= 15.00 ft3
/lbma
3-3 (a) SI Units -27 C, 1500 m elevation
P = 99.436 + 1500(-0.01) = 84.436 kPa
Pv = 3.60 kPa, Table A-1b
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19. 10
W =
0.6219x3.60
0.0277 kgv/kga
(84.436 3.60)
=
−
i = 27 + 0.0277 (2501.3 + 1.86 x 27) = 97.68 kJ/kga
3-3 (cont’d)
v =
3
0.287x300
1.065 m / kga
(84.436 - 3.60)
=
(b) SI Units – 0.0C; 1500m or 84.436 kPa
Pv = 0.61 kPa; Table A-1b
W =
0.6219 x 0.61
0.00453 kgv / kga
(84.436 - 0.61)
=
i = 0.0 + 0.00453 (2501.3 – 0.0 x 1.86) = 11.33 kJ / kga
v =
0.287 x 273
(84.436 - 0.61)
= 0.935 m3
/ kga
3-4 (a) English Units – 70F, Pv = 0.363 psia
Pv = φ Pg = 0.75(0.363) = 0.272 psia
W =
0.6219 (0.272)
0.0117 lbmv / lbma
(14.696 - 0.272)
=
i = 0.24 (70) + 0.0117 [1061.2 + 0.444 (70)] 29.58 Btu / lbma
=
(b) Pv = 0.75 (0.363) = 0.272 psia; P = 12.24 psia
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20. 11
W =
0.6219 (0.272)
(12.24 - 0.272)
= 0.0141 lbmv / lbma
i = 0.24(70) + 0.0141 [1061.2 + 0.444 (70)] 32.20 Btu/ lbma
=
3-4 SI Units –
(a) 20C, 75% RH, Sea Level
3-4 (cont’d)
Ps = 2.34 kPa; Pv = 0.75 x 2.34 = 1.755 kPa
0.6219 x 1.755
W = =
(101.325 - 1.755)
0.0110 kgv / kga
i = 1.0 t + W(2501.3 + 1.86t)
i = 20 + 0.0110(2501.3 + 1.86 x 20) = 47.92 kJ / kga
(b) 20C, 75% RH, 1525m
P = 99.436 – 0.01 x 1525 = 84.186 kPa
Ps = 2.34 KPa; Pv = 0.75 x 2.34 = 1.755 kPa
W =
0.6219 x 1.755
(84.186 - 1.755)
= 0.0132 kgv / kga
i = 20 + 0.0132(2501.3 + 1.86 x 20) = 53.51 kJ / kga
3-5 English Units –
t = 72 Fdb; psia
14.696
P
%;
50 =
=
φ
s
v
s
v
P
P
or
P
P
φ
φ =
= ; Pv = 0.5(0.3918) = 0.196 psia
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21. 12
Air dewpoint = saturated temp. at 0.196 psia = 52.6 F
Moisture will condense because the glass temp.
40 F is below the dew point temp.
3-5 SI Units – t = 22C ; 50% ; P = 100 kPa
Pv = φ Ps ; Pv = 0.5(2.34) = 1.17 kPa
3-5 (cont’d)
Air dewpoint = sat.temp. at 1.17 kPa = 9.17 C
Glass temp. of 4 C is below the dewpoint of 9.17 C, therefore,
moisture will ccondense on the glass
3-6 English Units -
(a) At 55F, 80% RH, va = 13.12 ft3
/ lba and ρ a = 0.0752 lbma / ft3
= 22,860 lbma / hr
a
m 5000 (0.0762) 381 lbma / min
= =
(b) Using PSYCH ρ a = 0.0610 lbma / ft3
or va = 16.4 ft3
/ lba
= 5000 (0.061) = 305 lbma / min
a
m
18,300 lbma / hr
=
3-6 SI Units –
(a) t = 13 C and relative humidity 80%
then va 0.820 m
≈ 3
/ kga; a
m 2.36 / 0.82 2.88 kga / s
= =
(b) Assuming same conditions
;
3
a
v 0.985 m / kga
= a
m 2.36 / 0.985 2.40 kga / s
= =
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22. 13
3-7 English Units – t = 80F, 60% RH
(a) v s
P P 0.6 (0.507) 0.304 psia
φ
= = =
= 64.5 F
dp sat v
t (t @ P
= )
(b) Same as (a) above
3-7 SI Units –
(a) 27 C, 60% RH, Sea Level
Ps = 3.57 kPa; Pv = 0.6 x 3.57 = 2.14 kPa
dp sat v
t =(t at P ) 18.4 C
≈
(b) Same as (a) above
3-8 dp
t 9C (48F)
≤
42%
φ ≤ ; W 0.0071 kgv / kga (lbv / lba)
≤
Chart 1a 1b
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23. 14
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
dp Room
Problem 3-8
W=0.0071
72 (22)
48 (9)
42 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
00
500
0
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-9 (a,b,d) Using the Properties option of PSYCH:
Relative Humidity = 0.59 or 59%
Enthalpy = 30.4 Btu/lbma
Humidity Ratio = 0.0114 lbu/lba
(c) Again using the Properties option
At W=0.0114 lbv/lba; RH = 1.00 or 100%
The dew point = tdb or twb = 59.9 F
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24. 15
3-9 (cont’d)
(e) Using the Density of Dry Air option:
Mass Density = 0.070 lba/ft3
3-10 Using program PSYCH
(a) tdb = 102.6; twb = 81.1F
75 Fdb; 65 fwb; 14.2 psia
(b) m 58.7
ν =
lbm/hr
Q
2 = 1027 cfm
3-11 t1 = 80 / 67 F; t2 = 55 F and sat.; assume std. barometer
(a) W1 – W2 = 0.0112 – 0.0092 = 0.002 lbv / lba
(b) l
q 31.5 - 29.3 2.2 Btu / lba
= =
(c) qs = 29.3 – 23.2 = 6.1 Btu / lba
(d) q = l s
q q 8.3 Btu / lba
+ =
3-12 (a) *
2
0.6219 (0.3095)
W 0.0134 kgv / kga
(14.696 0.3095)
= =
−
1
0.24 (65 - 80) ( 0.0134 x 1056.5)
W 0.00993 lbv / lba
(1096 - 33)
+
= =
also W1 = 0.6219 Pv1 / (P – Pv1)
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25. 16
Pv1 = (0.00993 x 14.696) / ( 0.6219 + 0.00993) = 0.231 psia
3-12 (cont’d)
1
0.231
0.46 or 46%
0.507
φ = =
(b) P = 29.42 – (0.0009 x 5000) = 24.92 in.Hg. or P = 12.24 psia
*
2
0.6219 x (0.3095)
W 0.01613
(12.24 - 0.3095)
= = lbv/lba
W1 =
0.24(65 80) (0.01613 x 1056.5)
0.01265 lbv / lba
( 1096 - 33)
− +
=
or kgv / kga
Pv1 = 0.01265 x 12.24 / ( 0.6219 + 0.01265) = 0.244 psia
1
0.244
0.48 or 48%
0.507
φ = =
3-13 (a) Sea Level
Dry
Bulb, F
Wet
Bulb, F
Dew
point
F
Humid.
Ratio, lba/lbv
Enthalpy
Btu/lba
Rel.
Humid., %
Mass
Density
lba/ft3
85 60 40.6 0.0053 26.6 21 0.072
75 59.6 49.2 0.0074 26.1 40 0.073
74.6 65.1 60.1 0.0111 30 60 0.073
88.6 70 60.9 0.01143 33.8 40 0.071
100 85.8 81.7 0.0235 50 56 0.068
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26. 17
(a) 5000 ft.
Dry
Bulb, F
Wet
Bulb, F
Dew
point
F
Humid.
Ratio, lba/lbv
Enthalpy
Btu/lba
Rel.
Humid., %
Mass
Density
lba/ft3
85 60 45.1 0.0076 28.7 25 0.060
75 58.6 49.2 0.0089 27.7 40 0.061
71.2 61.6 56.7 0.0118 30 60 0.061
102.7 70 55.8 0.01143 37.3 22 0.058
100 81.3 76.1 0.0235 50 47 0.057
(c) Note effect of barometric pressure.
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27. 18
3-14
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
dp Room
Problem 3-14
72 (22)
52 (11)
Max RH=49.6 %
W=0.0083
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-15 Use Chart 1b, SI
(a) td = 10 C; SHF = 0.62
(b) 1 2
2.4
q m (i i ) (57.1 - 34)
0.867
= − =
= 63.95 kJ / s = 63.95 k W
s
q 63.95 (0.62) 39.65 kW
= =
3-15 Use Chart 1a, IP
(a) td = 52 F; SHF = 0.63
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F
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28. 19
3-15 (cont’d)
(b)
5000(60)
q = (32 - 22.6)= 203,317. Btu/hr
13.87
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
1
ADP
2
Problem 3-15
80 (27)
55 (13)
52 (10)
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
s
q 203,317 (0.63) 128,089. Btu/hr
= =
3-16 (a) i1 = 30 Btu / lba; v1 = 13.78 ft3
/ lba; W = 0.0103
lba
lbv
; 50%
1 =
φ
(b) i1 = 51.6 kJ / kga
v1 = 0.86 m3
/ kga
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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29. 20
3-16 (cont’d)
W1 =
kga
kgv
0103
.
0
50%
1 =
φ
3-17 Use the Heat Transfer option of program PSYCH:
q = 148,239 Btu/hr
s
q 102,235 Btu/hr
=
SHF = 0.69
3-18 Use the Heat Transfer option of program PSYCH for sensible heat
transfer only:
s
q 178,911 Btu/hr
= −
Negative sign indicates heating.
3-19 Use the program PSYC to compute the various
properties at 85/68 F; sea level and
6000 ft elevation.
Elevation
ft
Enthalpy
Btu/lbm
Rel. Hum
percent
Hum. Ratio
lbv/lba
Density
lba/ft3
0 32.2 42 0.0107 0.072
6000 36.3 45 0.0144 0.058
At sea level: a
m 5000 x 0.072 x 60 21,600 lba/hr
= =
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30. 21
3-19 (cont’d)
At 6000 feet:: a
m 5000 x 0.057 x 60 17,100 lba/hr
= =
Percent Decrease at 6000 ft:
(21
,600 17,100)100
PD 20.8%
21,600
−
= =
3-20 Use the program PSYC to compute the heat transfer
rates at 1000 and 6000 feet elevation:
(a) at 1000 ft, q 200,534 Btu/hr
=
(b) at 6000 ft, q 190,224 Btu/hr
=
(c) PD =
(200,534 190,224)100
5.1 %
200,543
−
=
3-21 (a) English Units –
; = 0
in.Hg.
29.92
PB =
q
w
i
i 180.2 0.8 (970.2)
W
∆
= = +
∆
iw = 956.4 Btu / lbv
From chart 1a; t2 = 91.5 F
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
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31. 22
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
T
EMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
1
2
Problem 3-21
98 (38)
91.5 (32)
60 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-21 (a) SI Units –
PB = 101.325 kPa
w
i
i 419.04 (0.8x2257)
W
∆
= = +
∆
iW = 2224.6 kJ / kg
From chart 1b; t2 = 32 C
(b) Use Humidification (adiabatic) option to obtain 91.5 F db.
3-22 PB = 29.92 in.Hg.; 0
q =
(a) Using chart 1a
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F
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32. 23
3-22 (cont’d)
w
i
i 1090 Btu / lbm
W
∆
= =
∆
From table A-1
f
fg
i-i 1090 - 196.1
x =
i 960.
=
1
x = 0.931 or about 93 %
(b) x will be the same
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
1
a
b
Problem 3-22
80
60
1090
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
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R
33. 24
3-23 Assume PB = 101.325 kPa; 0
q =
w
∆i 272.1
i kJ / kg
∆W 1000
= =
iw = 0.272 (on scale)
t2 = 22.6 C
10 20 30 40 50
60
70
80
90
100
110
110
120
120
ENTHALPY - KJ PER KILOGRAM OF DRY AIR
10
20
30
40
50
60
70
80
90
100
E
N
T
H
A
L
P
Y
-
K
J
P
E
R
K
I
L
O
G
R
A
M
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
C
5
10
15
20
2
5
30
35
40
45
50
D
RY
BU
LB
TEMPERA
TU
RE
-
°C
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
10% RELATIVE HUMID ITY
20%
30%
40%
50%
60%
70%
80%
90%
5
5
10
10
15
15
20
20
25
25
30 WET BULB TEMPERATURE - °C
30
0
.7
8
0
.8
0
0
.8
2
0
.
8
4
0
.8
6
V
O
L
U
M
E
-
C
U
B
IC
M
E
T
E
R
P
E
R
k
g
D
R
Y
A
IR
0
.8
8
0
.9
0
0
.9
2
0
.9
4
HUMI
DITY
RATIO
-
GRAM
S
M
OISTURE
PER
KI
LOGR
AM
D
RY
AIR
1
2
Problem 3-23
38
22.6
20
80 %
0.272
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 101.325 kPa
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
1.5
2.0
4.0
-4.0
-2.0
-1.0
-
0
.5
-0
.2
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.7
0.8
-5.0
-2.0
0.0
1.0
2
.0
2.5
3
.0
4
.
0
5
.0
10
.0
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-24 For adia. humidification
(a) w
∆i
= i 1131 Btu / lbw
∆W
=
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34. 25
3-24 (cont’d)
c a 2
q = m (i - i )
1
a
m 2000x60/13.14
=
a
m 9132 lba / hr
=
1 2
i 18.1 Btu / lba ; i 29.7 Btu / hr
= =
c
q 9132 (29.7 - 18.1) 105,931 Btu / hr
= =
w a 3 2 3 2
m m (W - W ) ; W = 0.0167; W 0.0032 lbv/lba
= =
w
m 9132 (0.01 67 - 0.0032) 123.3 lbw / hr
= =
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35. 26
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
TEMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
1
2
3
Problem 3-24
1131
30 %
110 (43)
60 (16)
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
(b) Solution similar to (a)
3-25 English Units –
See diagram for construction on chart 1a.
1
3
Q
32 2000 2
=
3000 3
Q
12
= =
Layout 2L/3 on the chart and read:
W3 = 0.007 lbv/lba
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
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36. 27
I3 = 22.2 Btu/lba
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
TEMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
1
2
3
Problem 3-25
40 (4) 100 (38)
58.4 (15)
35
77
52
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-25 SI Units – Same procedure as above, read:
3
i 34 kJ / kga
=
3
W 0.007 kgv / kga
=
3-26 English Units –
Layout the given data on Chart 1a as shown for problem 3-25.
a1
m 2000(60) 12.66 9,479lba hr
= =
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37. 28
3-26 (cont’d)
a2
m 1000(60) 14.44 4,155lba hr
= =
a1
a1 a2
m
32 9479
= 0.695
m +m 9479 4155
12
= =
+
Layout distance 32 on line from 1 to 2 to locate point 3 for the
mixture.
Read: i3 = 21.5 Btu/lbm
W3 = 0.0067 lbu/lba
For W, % Error =
(0.007 0.0067)100
4.5
0.0067
−
=
For I, % Error =
(22.2 21.5)100
3.3
21.5
−
=
3-27
250,000
SHF 0.8
200,000
= =
or SHF =
59
.81
73
=
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F
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38. 29
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
T
EMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
1
2
Problem 3-27
75 (24)
50 %
53 (12)
0.8
21.5
28.2
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.
4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-28 Refer to diagram for 3-27
(a) a 1 2 1 2
q = m (i - i ); i 28.2; i 21.5
= =
a
m 250,000 / (28.2 - 21.5) 37,313 lba / hr
= =
3
a 2
Q = m v 37,313 x 13.09 / 60 8,140 ft / min
= =
(b) similar procedure;
3
Q 3.85 m / s
=
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39. 30
3-29 (a) Use the AirQuantity option of program PSYCH, iterating on the
relative humidity and setting the minimum outdoor Air Quantity to
0.01, NOT ZERO.
Use the properties option to find the entering wet bulb
temperature of 62.6F. Then
φ = 0.852 (iterated)
ts = 56F
= 9,360 cfm
s
Q
(b) Proceed as above
φ = 0.882
ts = 56F
= 10,014 cfm
s
Q
3-30 Proceed as in 3-29 above.
φ = 0.92
ts = 56.1 56 F
≈
= 11,303 cfm
s
Q ≤
3-31 (a) 91
.
0
000
,
550
000
,
500
SHF =
=
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students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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40. 31
3-31 (cont’d)
(b) a 2 1
q = m (i -i )
or a 2
m = q/(i -i )
1
a
550,000
m
(34.3 22.8)
=
−
a
m =47,826lba hr
a 2
2
m v 47,826
Q = = x 14.62=11,654 cfm
60 60
or 5.5 m3
/s
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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41. 32
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
TEMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
1
2
Problem 3-31
0.91
115 (46)
72 (22)
30 %
22.8
34.3
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.
4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
500
0
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-32 a 2 1
q = m (i -i )
2
a
q
i = +i
m
1
a
1400 x 60
m 5,915.5
14.2
=
2
-5 x 12,000
i = +38.5
5,915.5
Btu/lba
2
i 28.3
= 6
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students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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6
F
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42. 33
Then from Chart 1a, t2= 67F
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
1
2
ADP
Problem 3-32
90
75
67
28.4
55
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-33 Use Adiabatic Mixing option of PSYCH with the Properties option to
enter requested data. Assume volume flow rates of 3 to 1 to obtain.
Tmix,db = 84.2 F
Tmix,wb = 71.3 F
3-34 Use Program PSYCH at Sea Level elevation
Iteration on the supply volume flow rate is required. This is the same as the
leaving air quantity for the coil.
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1
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F
M
R
43. 34
3-34 (cont’d)
(a) Supply air quantity is 9,384 cfm.
(b) The outdoor air quantity is 938 cfm.
(c) Air enters the coil at 74.6 F db, 60.5 F wb at a rate of 9,740 cfm
(d) The coil capacity is 248,256 Btu/hr.
The amount of air returned is: (9,740 – 939) = 8,802 cfm.
3-35 Use Program PSYCH at 5,000 ft elevation
Iteration on the supply volume flow rate is required. This is the same as the
leaving air quantity for the coil.
(a) Supply air quantity is 11,267 cfm.
(b) The outdoor air quantity is 1,127 cfm.
(c) Air enters the coil at 74.6 F db, 62.1 F wb at a rate of 11,697 cfm
(d) The coil capacity is 334,143 Btu/hr.
The amount of air returned is: (11,697 – 1,127) = 10,570 cfm.
3-36 cfm
1000
Q0 =
(a) From Chart 1a
s
t =120/74 F
s
s r
q 200,000
m =
(i -i ) (37.2 22.8)
=
−
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M
1
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F
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R
44. 35
= 13,889 lb/hr = 1
m
3
s s s s
Q = m v = m (14.78)/60 = 3,421 ft /min
(b) o o o
m = Q /v 1000 x 60 / 12.61 4758 lb/hr
= =
r
1
m 13,889 4758
0.66;
m 13,889
−
= =
1
From Chart 1a t 61/ 47 F
=
3 1
t - t (119 61)
= −
(c) w s s 2
m = m (W -W ) 13,889 (0.0075 - 0.0036)
=
= 54.2 lbm/hr
(d) f 1 3 1
q = m (i -i ) =13,889 (32.8 18.6) 197,224 Btu/hr
− =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M
1
6
F
M
R
45. 36
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
r
s
0
1
3
1 3
Problem 3-36
120
72
30 %
40 61
47
0.8
1150
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-37 (a) s
t 120 / 71.4 F Use Chart 1Ha
=
s 1
m 200,000 /(38.7 24.0) 13,605 lba/hr m
= − =
=
s
Q 13,605 x 17.85 / 60 4048 cfm
= =
(b) lba/hr
3947
60
x
)
2
.
15
/
1000
(
m0 =
=
r
1
1
m 13,605 3947
0.71; t 62.8/ 47 F
m 13,605
−
= = =
3 1
t -t (119.5 62.8)
= −
(c) w s s 1
m =m (w -W ) 13,605 (0.0088 - 0.0046) 57.14 lbw/hr
= =
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students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M
1
6
F
M
R
46. 37
(d) f
q 13,605 (33.8 - 20.2) 185,028 Btu/hr
= =
3-38 Assume fan power and
heat gain are load on the space
s
9384
m x 60 = 42,915 lbm/hr; Prob 3-34
13.12
=
fan duct s s c
W q m (i i
+ = −
)
= (4 x 2545) + 1000 = 11,180 Btu / hr
c
11
,180
i 20.8 20.54 Btu/lbm
42,915
= − =
State c is required condition leaving coil
Part a, b, and c are same as prob. 3-34;
(d) coil 1 1 c
q =m (i -i ) 42,915 (26.8 - 20.54) 268,648 Btu/hr
= =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M16FMR
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USE IT WITH YOUR MIND
M
1
6
F
M
R
47. 38
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
s
r
0
1
c
1
Problem 3-38
100
72
55
20.54
50 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-39 )
i
i
(
m
W
);
i
i
(
m
q c
s
s
fan
s
r
s
r −
=
−
=
(a) c r
i 28 Btu/lbm; i 33.7 Btu/lbm
= =
Using Chart 1Ha
r
q 1,320,000 Btu/hr
=
fan
W 30 x 2545 76350 Btu/hr
= =
fan a s c
W 30 x 2545 76,350 = m (i -i )
= =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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USE IT WITH YOUR MIND
M
1
6
F
M
R
48. 39
s a
q = 1,320,000 = m r s
(i -i )
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35 40
40 45
45 50
50
55
55
60
60
65
65
70
70
75
75
80 WET BULB TEMPERATURE - °F
80
85
1
5
.5
1
6
.0
1
6
.5
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
7
.0
1
7
.5
1
8
.0
HUMIDITY
RATIO
-
POUNDS
MOISTURE
PER
PO
UND
DRY
AIR
r
0
c
s
s
Problem 3-39
90 (32)
80 (27)
50 %
59 (15)
62.5 (17)
0.8
R R
ASHRAE PSYCHROMETRIC CHART NO.4
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 24.896 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
5000 FEET
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-0
.4
-
0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
10
00
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
Two unknowns two equations
Solve simultaneous:
fan s a r c
a
a
W +q = m (i -i )
1,320,00+76,3 50
m =
(33.7-28)
m =244,974lba/hr
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M
1
6
F
M
R
49. 40
s r s a
i = i - (q m )
s
1,320,000
i = 33.7 - =28.3
244,974
Btu/lba
Locate points on the condition line on Chart 1 Ha and point c is on
cooler process line horz. to left of points.
Read ts = 62.5 F, tc = 61.6F.
(a) s
244,974
Q = x16.2 = 66,143cfm
60
(b) 3
s
Q 31.2 m
=
s
H
3-40 English Units –Tucson, Arizona, Elevation 2,556 ft.
;
min 0
i =i =31.1 Btu/lba and sat. air min
t =64.5 F; PSYCH
Shreveport, Louisiana, Elevation 259 ft.
;
min 0
i =i = 42.5 Btu/lba and sat. air min
t 76.8 F; PSYC
=
SI Units – Tucson, Arizona
;
min 0
i =i 51.5 kJ/kga
= min
t =18.1 C; Chart 1b
Shreveport, Louisiana
;
min 0
i =i =75.5 kJ/kga min
t =24.8 C; Chart 1b
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M16FMR
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USE IT WITH YOUR MIND
M
1
6
F
M
R
50. 41
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
3
.0
1
3
.
5
1
4
.
0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
I
R
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
SL
TLO
Problem 3-40
Shreveport, LA
95
76.8
R R
ASHRAE PSYCHROMETRIC CHART NO.4
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.642 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
259 FEET
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-0
.4
-
0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
10
00
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
M16FMR
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USE IT WITH YOUR MIND
M
1
6
F
M
R
51. 42
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.00 2
.00 4
.00 6
.00 8
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40 45
45 50
50 55
55
60
60
65
65
70
70
75
75
80 WET BULB TEMPERATURE - °F
80
85
85
1
4
.0
1
4
.
5
1
5
.
0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
I
R
1
5
.5
1
6
.0
1
6
.
5
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
TA
TLO
Problem 3-40
Tucson, Arizona
102
64.6
R R
ASHRAE PSYCHROMETRIC CHART NO.4
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 27.259 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
2556 FEET
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-0
.4
-
0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
10
00
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-41 )
i
i
(
m
q s
r
s −
=
(a) = 1,319 lba/hr ton
s
m 12,000 /(28.2 19.1)
=
−
s
1319 x 15.6
Q 343 cfm/ton
60
= =
o
s
m r1 13
= 0.55 or 55%
m 23.5
r0
= =
(b) 3
s
Q 0.046 m / s - kW
≈
0 s
m /m 55%
≈
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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USE IT WITH YOUR MIND
M
1
6
F
M
R
52. 43
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35 40
40 45
45 50
50
55
55
60
60
65
65
70
70
75
75
80 WET BULB TEMPERATURE - °F
80
85
1
5
.5
1
6
.0
1
6
.5
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
7
.0
1
7
.5
1
8
.0
HUMI
DITY
RATIO
-
POUNDS
MOISTURE
PER
POUND
DRY
AIR
r
s
0
1
Problem 3-41
100 (38)
75 (24)
50 (10)
10 %
40 %
0.7
R R
ASHRAE PSYCHROMETRIC CHART NO.4
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 24.896 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
5000 FEET
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-0
.4
-
0
.3
-0
.2
-0.
1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
10
00
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-42 2 2 3 2
500,000
q m (i i ); m
(41.1 21.9)
= − =
−
lba/hr
042
,
26
m2 =
= 6315 cfm
14.55/60
x
26042
Q2 =
lba/hr
6511
26,042
x
25
.
0
m0 =
=
F
5
.
49
/
5
.
67
t
;
25
.
0
m
/
m mix
3
0 =
=
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
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1
6
F
M
R
53. 44
3-42 (cont’d)
Preheat Coil:
ph 0 p 4 0
q = m c (t -t ) 6511 x 0.24 (60-6) 84,383 Btu/hr
= =
Heat Coil:
h 2 5 1
q = m (i -i ) 26,042 (28.4 - 20) 218,753 Btu/hr
= =
Humidifier:
w 2 2 5
m = m (W -W ) 26,042 (0.0144 - 0.0035)
=
283.9 lbw/hr
=
(b) 3
2 ph h
Q 2.98 m / s; q 24.7 kW; q 64.1 kW;
= = =
kg/s
036
.
0
mw =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
M16FMR
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USE IT WITH YOUR MIND
M
1
6
F
M
R
54. 45
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
TEMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
3
2
4
1
5
2
Problem 3-42
1153
70 (21)
30 %
105 (40)
60 (16)
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIB LE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HU MIDITY RATIO
'h
'W
3-43 Use Chart 1a; d a r
q m (i is)
= −
or )
i
i
/(
q
m s
r
d
a −
=
(a) m
a = 150 x 12,000 / (28.4-22) = 28,125 lbm/hr
d
Q 28,125 x 13.25/60 61,211 cfm
= =
m d
Q 0.20 Q 1,242 cf
= =
m
m m
m = 1
,242 x 60/13.5 5,521 lbm/hr [v assumed]
=
m r m
i =i 1.8 x 12,000/5,521 24.5 Btu/lbm; t 62 / 57 F
− = =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M16FMR
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USE IT WITH YOUR MIND
M
1
6
F
M
R
55. 46
(b) 3 3
d m m
Q = 2.93 m /s; Q = .59 m /s; t = 17/14 C
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
r
m
s
Problem 3-43
0.8
0.6
75 (24)
60 (16)
62 (17)
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-44 (a) a
15.0 x 12,000
m 29,508 lba/hr
(31.2 - 25.1)
= =
d m
Q 29,508 x 16.0/60 7,869 cfm; Q = 0.2 x Q
= =
s
1,574 cfm
=
m m
m =1
,574 x 60/16.2 5,829 lba/hr (v assumed)
=
m
i 35.7 1.8 x 12,000/5,829 27.5 Btu/lba;
= − =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
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USE IT WITH YOUR MIND
M
1
6
F
M
R
56. 47
m
t 62.5/58 F
=
(b) 3 3
s m m
Q =3.7 m / s; Q 0.74 m /s; t 17 /14.4 C
= =
3-45 Use Chart 1a; r
1
m 10
0.8
m 0r
= =
[Both design and min. load condition]
is = ir - /
m
q
s
m
s
r
d
s
i
i
Q
m
−
=
=
22.3)
-
(29.35
12,000
x
50
conditions
all
for
constant
is
m
lba/hr;
106
,
85
m s
s
=
Btu/lba
25.83
106
12,000/85,
x
25
35
.
29
i '
s =
−
=
(a) From Chart 1a; F
64
t '
s =
(b) s'
b
c
'
1
b
s
s i
)
m
m
(
i
m
i
m
+
=
+
271
.
0
7
.
31
8
.
25
8
.
25
2
.
24
)
i
i
(
)
i
i
(
m
m
'
1
'
s
'
s
s
c
b
=
−
−
=
−
−
=
(b) From chart 1a; cases
both
for
F
49
td =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
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USE IT WITH YOUR MIND
M
1
6
F
M
R
57. 48
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
r
s
0
1
s
0'
1'
s
s'
Problem 3-45
0.9
95 (35)
85 (29)
77 (25)
64 (18)
55 (13)
50 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-46 Refer to problem 3-45. Results are similar.
3-47 (a) It is probably impossible to cool the air from 1 to 2 in one
process. The extension of line 12 does not intersect the
saturation curve.
(b) Cool the air to state 1' and then heat to state 2.
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
M16FMR
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USE IT WITH YOUR MIND
M
1
6
F
M
R
58. 49
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
TEMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
1
2
1'
2
Problem 3-47
80 (27)
60 (16)
52 (11)
67
54
90 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-48 (a)
c
s
m sh
= =.83
m ch
7
h
s
m cs
= 0.16
m ch
=
3
c
h
m 0.837
5.14
m 0.163
= =
s r s
q m (i i
= −
)
s
50 x 12,000
m 93,750 lba/hr
(28.2-21.8)
= =
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students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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1
6
F
M
R
59. 50
s
Q 93,750 x 13.2/60 20,625 cfm
= =
(b) 3
s
Q 9.7 m /
=
s
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
r
c
h
s
Problem 3-48
90 (32)
75 (24)
52 (11)
90 %
0.65
20 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0.
1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-49 See diagram of problem 3-48
(a) c h
s s
m m
36 10.1
0.9; 0.10
m 46.3 m 46.3
= = = =
; c
h
m 0.9
9.0
m 0.10
= =
s
50 x 12,000
m 83,333 lba/hr
(30.1 - 22.9)
= =
s
Q =83,333 x 15.67/60 21,763 cfm
=
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
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F
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R
60. 51
(b) 3
s
Q =10.3 m /s
3-50 (a) See diagram for problem 3-48
c
c c r c c s
s
m
= 0.837; q = m (i -i ); m 0.714 x m 0.837 x 93,750
m
= =
;
c
m 78,469 lba/hr
=
c
Q 78,469 x 13.04/60 17,054 cfm
= =
c
q 78,469 (28.2-20.6) 596,364 Btu/hr
= =
(b) 3
c c
Q =8.1 m /s; q 175 kW
=
3-51 SI Units
(a) On the basis of volume flow rate using Chart 1b:
2 3
13
Q = Q 0.69 x 1.18 0.815
12
= =
m3
/s
and m
1 3 2
Q = Q - Q = 1.18 0.815 0.365
− =
3
/s
(b)
3
34 a3 4 3 4 3
3
34
Q
q = m (i -i ) = (i -i )
v
1.18
q = (47.8-41.0) = 9.6 kW
0.835
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M
1
6
F
M
R
61. 52
10 20 30 40 50
60
70
80
90
100
110
110
120
120
ENTHALPY - KJ PER KILOGRAM OF DRY AIR
10
20
30
40
50
60
70
80
90
100
E
N
T
H
A
L
P
Y
-
K
J
P
E
R
K
I
L
O
G
R
A
M
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
C
5
10
15
20
2
5
30
35
40
45
50
D
RY
BU
LB
TEMPERA
TU
RE
-
°C
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
5
5
10
10
15
15
20
20
25
25
30 WET BULB TEMPERATURE - °C
30
0
.7
8
0
.8
0
0
.8
2
0
.
8
4
0
.8
6
V
O
L
U
M
E
-
C
U
B
IC
M
E
T
E
R
P
E
R
k
g
D
R
Y
A
IR
0
.8
8
0
.9
0
0
.9
2
0
.9
4
HUMIDITY
RATIO
-
G
RAM
S
M
OISTURE
PER
KILOGR
AM
D
RY
AIR
1
2
3 4
Problem 3-51
Problem 3-51
29
24
17.2
12
50 %
11
14.7
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 101.325 kPa
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
1.5
2.0
4.0
-4.0
-2
.0
-1.0
-0
.5
-0
.2
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.7
0.8
-5.0
-2.0
0.0
1.0
2
.0
2.5
3
.0
4
.
0
5
.0
10
.0
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
English Units
(a) 1 34
Q = 640 cfm; q = 33,684 Btu/hr
3-52 (a),(b)
From Chart 1b, states 1.4 and ADP are known. Based on approx.
11.8 C db, 11.2 C wb, and 90% RH locate state 2.
Then for full load design condition air is cooled from 1 to 2 and the
room process proceeds from 2 to 4.
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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1
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F
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R
62. 53
For the high latent load condition, the air at 2 is reheated to state 3
where it enters the space and the process proceeds to state 4.
(c) 2
24 a 4 2 4 2
2
Q
q = m (i -i ) = (i -i )
v
2
Q =35 x 0.817 (47.7-32)
; m
2
Q 1.8
=
2 3
/s
12 a 1 2
12
1.82
q = m (i -i ) = (60.6-32)
0.817
q = 63.7 kW
34 a 4 3
34
23 24 34
1.82
q = m (i -i )= (47.7-39.4)
0.817
q = 18.5 kW
q = q - q = 35-18.5=16.5 kW
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
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M
1
6
F
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R
63. 54
10 20 30 40 50
60
70
80
90
100
110
110
120
120
ENTHALPY - KJ PER KILOGRAM OF DRY AIR
10
20
30
40
50
60
70
80
90
100
E
N
T
H
A
L
P
Y
-
K
J
P
E
R
K
I
L
O
G
R
A
M
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
C
5
10
15
20
2
5
30
35
40
45
50
D
RY
BU
LB
TEMPERA
TU
RE
-
°C
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
10% RELATIVE HUMID ITY
20%
30%
40%
50%
60%
70%
80%
90%
5
5
10
10
15
15
20
20
25
25
30 WET BULB TEMPERATURE - °C
30
0
.7
8
0
.8
0
0
.8
2
0
.8
4
0
.8
6
V
O
L
U
M
E
-
C
U
B
IC
M
E
T
E
R
P
E
R
k
g
D
R
Y
A
IR
0
.8
8
0
.9
0
0
.9
2
0
.9
4
HUMIDITY
RATIO
-
GRAM
S
M
OISTURE
PER
KILOGR
AM
D
RY
AIR
1
ADP 2 3
4
3
Problem 3-52
Problem 3-52 21
27
23
17
19
14
11.8
11
9
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 101.325 kPa
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
1.5
2.0
4.0
-4.0
-2.0
-1.0
-
0
.5
-0
.2
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.7
0.8
-5.0
-2.0
0.0
1.0
2
.0
2.5
3
.0
4
.
0
5
.0
10
.0
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-52 English Units
(a),(b) See above
(c) Btu/hr
2
Q = 4103cfm ;
12
q =221,243
Btu/hr;
34
q 67,49
=
8 2
23
q 52,50
=
Btu/hr
3-53 English Units
(a) s r s s
q=m (i -i ); m 5000 x 60/13.2 22,727 lba/hr
= =
(specific volume value of 13.2 ft3
/lbm is assumed.)
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M
1
6
F
M
R
64. 55
s r s
i = i - q /m =28.2 10 x 12,000 / 22,727 22.9 Btu/lba
− =
s o s o
t = t = 57.5 F; W =W 0.0083 lbv/lba
=
(b) r r
m s
m m
0m
= = 0.462
m m
0r
r
m =0.462 x 22,727 10,500 lba/hr
=
o
m 22,727 10,500 12,227 lba/hr
= − =
r
Q 10,500 x 13.68/60 2,394 cfm
= =
o
Q 12,227 x 12.11/60 2,468 cfm
= =
(c)
r
m'
m 0'm'
= =0.578
m 0'r
r o
m =0.578 x 22,727 13,131 lba/hr; m 9,596 lba/hr
= =
'
r o'
Q =13,131 x 13.68/60 2,994 cfm; Q 9,596 x 13.48/60
= =
= 2,156 cfm
(d) c s m' s
q = m (i -i ) 22,727 (28.4 - 22.8) 127,271 Btu/hr
= =
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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USE IT WITH YOUR MIND
M
1
6
F
M
R
65. 56
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
TEMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMIDITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
r
0
m
s
0'
r
m'
ADP
Problem 3-53
0.8
1150
75 (24)
70 (21)
65 (18)
57.5 (14)
40 (4)
43 (6)
90 %
50 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-53 SI Units
(a) ts = 14.2C; Ws = 0.0083 kgv/kga
(b)
3
r
Q =1.13m s
;
3
o
Q =1.17m s
(c)
3
r
Q =1.41m s
;
3
o'
Q =1.02m s
(d) c
q = 37.3 kW
3-54 (a) Any combination that will yield
an enthalpy less than 57.0 kJ/kga or 33 Btu/lba
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to
students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted
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M
1
6
F
M
R
66. 57
(b) r
s m
kga/s
95
.
5
84
.
0
/
5
m
=
=
=
o
r
m mr
= =0.36
m 0r
o
m 0.36 x 5.95 2.14 kga/s
= =
3
o
Q = 2.14 x 0.852 = 1.82 m /s = 3,857cfm
(c) ad
t 15.4 C or 60F
=
(d) (Essentially, no difference)
o n m s r s
q /q = (i -i )/(i -i ) = 1.0
10 20 30 40 50
60
70
80
90
100
110
110
120
120
ENTHALPY - KJ PER KILOGRAM OF DRY AIR
10
20
30
40
50
60
70
80
90
100
E
N
T
H
A
L
P
Y
-
K
J
P
E
R
K
I
L
O
G
R
A
M
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
C
5
10
15
20
2
5
30
35
40
45
50
D
RY
BU
LB
TEMPERA
TU
RE
-
°C
2
4
6
8
10
12
14
16
18
20
22
24
26
28
30
10% RELATIVE HUMID ITY
20%
30%
40%
50%
60%
70%
80%
90%
5
5
10
10
15
15
20
20
25
25
30 WET BULB TEMPERATURE - °C
30
0
.7
8
0
.8
0
0
.8
2
0
.
8
4
0
.8
6
V
O
L
U
M
E
-
C
U
B
IC
M
E
T
E
R
P
E
R
k
g
D
R
Y
A
IR
0
.8
8
0
.9
0
0
.9
2
0
.9
4
HUMIDITY
RATIO
-
G
RAM
S
M
OISTURE
PER
KI
LO
GR
AM
D
RY
AIR
r
s
0
m
s
Problem 3-54
25 (77)
18 (64)
20 (68)
0.6
57
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 101.325 kPa
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
1.5
2.0
4.0
-4.0
-2.0
-1.0
-0
.5
-0
.2
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.7
0.8
-5.0
-2.0
0.0
1.0
2
.0
2.5
3
.0
4
.
0
5
.0
10
.0
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
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67. 58
3-55
424,000
SHF
530,000 424,000
−
=
−
= -4
Construct condition line on
Chart 1a with preheat and
mixing processes.
(a) sen s p r s
q = -424,000 = m c (t -t )
s
424,000
m 88,333 lba/hr
0.24 (75 95)
−
= =
−
3
s
Q =88,333 x 14.07/60 20,714 cfm or 9.8 m /s
=
(b)
r
r
m
m hm
= =0.33; m 0.33 x 88,333 lba/hr
m hr
=
r r
m =29,150 lba/hr; Q 29,150 x 13.68/60
=
3
6,646 cfm or 3.14 m /s
=
h
h
m
m
=1 0.33 0.67; m 0.67 x 88,333
m
− = =
h h
m 59,183 lba/hr; Q 59,183 x 13.1/60
= =
3
h
Q 12,922 cfm or 6.1 m /s (at heated condition)
=
(c) ph h p h o
q =m c (t -t ) = 59,183 x 0.24 (60-35)
q=355,098 Btu/hr or 104 kW
(d) m
q =88,333 x 0.24 (95 - 65) 635,998 Btu/hr or 186 kW
=
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68. 59
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
POUND
DRY
AIR
r
0 h
m
s
s
Problem 3-55
-4
95 (35)
75 (24)
50 %
60 (16)
35 (2)
20 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-56 Refer to chart 1a.
(a)
34 a3 4 3 3 4 3
3
34 3
3
4 3
3
3
60
q = m (i -i ) = Q x (i -i )
v
q v (1750 x 13.23)
Q x =
60(i -i ) 60(28.1-23)
Q = 75.7 or 76 cfm = 0.040 m /s
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69. 60
(b) t3db = 58.5 F and 80% RH or 15 C
(c)
3
2 3
31
Q = ; Q = 0.754 x 75.7 = 57 cfm or 0.028 m /s
12
3
1
Q = 76 - 57 = 19 cfm or 0.012 m /s
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BT U PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
T
EMPERAT
UR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
1
2
3
4
Problem 3-56
84
70
75
62
58.5
50
90 %
50 %
0.8
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-57 (a) Refer to Chart 1
A reheat system is required. Process 1-2 is for the coil. Process 3-4
is defined by the SHF = 0.5
Process 2-3 represents the required heat.
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70. 61
State 3 is defined by the intersection of the reheat and space
condition lines.
(b)
3
34 a3 4 3 4 3
3
34 3
3
4 3
3
3
Q x 60
q = m (i -i ) = (i -i )
v
q v 100,000 x 13.4
Q = =
60(i -i ) 60(28.2-23.9)
Q = 5,194 cfm or 2.5 m /s
(c)
12 a 1 2
12
23
23
5,194 x 60
q = m (i -i ) = (34.2-20.2)
13.4
q = 325,594 Btu/hr or 95.4 kW
5,194 x 60
q = (23.9-20.2)
13.4
q =86,050 Btu/hr or 25.2 kW
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71. 62
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BULB
TEMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE H UMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35
40
40
45
45 50
50 55
55 60
60
65
65
70
70
75
75
80
80
85 WET BULB TEMPERATURE - °F
85
90
1
2
.
5
1
3
.
0
1
3
.5
1
4
.0
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
4
.5
1
5
.0
HUMI
DITY
RATIO
-
POUN
DS
MOISTURE
PER
PO
UND
DRY
AIR
1
2 3
4
ADP
Problem 3-57
85
70
75
62
66
56
51
45
50 %
R R
ASHRAE PSYCHROMETRIC CHART NO.1
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 29.921 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
SEA LEVEL
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-0
.5
-
0
.4
-0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
1
000
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
3-58 Assume room temperature humidity of 50%
and layout the state
processes on
required from point c to s.
Supply Air:
=
sen
q 120,000 x 0.5 60,000 Btu/hr
= =
s p s r
m c (t -t )
s
60,000
m 53,192 lba/hr
0.24 (75-70.3)
= =
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72. 63
3
s
Q =53,192 x 16.33/60 14,477 cfm or 6.8 m /s
=
Mixed Air:
o
m 53,192 x 0.333 17,703 lba/hr
= =
3
o
Q 17,713 x 17.2/60 5,078 cfm or 2.4 m /s
= =
r
m 53,192 17,713 35,479 lba/hr
= − =
3
r
Q =35,479 x 16.5/60 9,757 cfm or 4.6 m /s
=
Reheat:
rh c p s c
q = m c (t -t ) 53,192 x 0.24 (70.3-55.2)
=
192,768 Btu/hr or 56.5 kW
=
Coil:
c m m c
q =m (i -i ) 53,192 (34.4 - 24.2)
=
542,558 Btu/hr or 159 kW
=
= %
1
.
5
412
,
200
100
)
109
,
190
412
,
200
(
=
−
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73. 64
10 15 20 25
30
35
40
45
50
55
55
60
60
ENTHALPY - BTU PER POUND OF DRY AIR
15
20
25
30
35
40
45
50
E
N
T
H
A
L
P
Y
-
B
T
U
P
E
R
P
O
U
N
D
O
F
D
R
Y
A
I
R
S
A
T
U
R
A
T
I
O
N
T
E
M
P
E
R
A
T
U
R
E
-
°
F
35
40
45
50
55
6
0
65
70
7
5
8
0
8
5
9
0
95
100
105
110
115
12
0
DR
Y
BUL
B
T
EMPERATUR
E
-
°F
.002
.004
.006
.008
.010
.012
.014
.016
.018
.020
.022
.024
.026
.028
10% RELATIVE HUMIDITY
20%
30%
40%
50%
60%
70%
80%
90%
35
35 40
40 45
45 50
50
55
55
60
60
65
65
70
70
75
75
80 WET BULB TEMPERATURE - °F
80
85
1
5
.5
1
6
.0
1
6
.5
V
O
L
U
M
E
-
C
U
.F
T
.
P
E
R
L
B
.
D
R
Y
A
IR
1
7
.0
1
7
.5
1
8
.0
HUMIDITY
RATIO
-
POUNDS
MOISTURE
PER
PO
UND
DRY
AIR
r
0
m
c s
s
Problem 3-58
90 (32)
75
75 (24)
50 %
70 (21)
55 (13)
90 %
0.6
0.5
R R
ASHRAE PSYCHROMETRIC CHART NO.4
NORMAL TEMPERATURE
BAROMETRIC PRESSURE: 24.896 INCHES OF MERCURY
Copyright 1992
AMERICAN SOCIETY OF HEATING, REFRIGERATING AND AIR-CONDITIONING ENGINEERS, INC.
5000 FEET
0
1.0 1.0
2.0
4.0
8.0
-8.0
-4.0
-2.0
-1.0
-
0
.5
-0
.4
-
0
.3
-0
.2
-0
.1
0
.1
0
.2
0
.
3
0.4
0.5
0.6
0.8
-2000
-1000
0
500
10
00
1
5
0
0
2
0
0
0
30
0
0
50
00
-
SENSIBLE HEAT Qs
TOTAL HEAT Qt
ENTHALPY
HUMIDITY RATIO
'h
'W
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74. Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for
testing or instructional purposes only to students enrolled in courses for which the textbook has been
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Requests for permission or further information should be addressed to the Permission Department, John
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Chapter 4
4-1 (a) comfortable
(b) too warm
(c) comfortable
(d) too dry
4-2 (a) comfortable
(b) too warm
(c) comfortable
(d) too dry
4-3 (a) Assume sedentary dry bulb of 78 F, clo = o.5, met. = 1.8;
using equation 4-4a, to,act. = 75 – 5.4(1 + 0.5)(1.8 – 1.2) = 71 F
Relative humidity should be less than 50%
(b) Should wear a sweater or light jacket and slacks.
(clo = 0.8)
4-4 Use fig 4-1
(a) Summer, to = 76 F or 24 C; Winter, to = 72 F or 22 C
(b) Use equation 4-4a as a guide, with clo = 0.2,
met = 3.0, db
t 76
= F
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