This paper is intended to promote two (2) concepts, advection, and heat flux. Advection is the transport of thermal energy via a moving (working) fluid and heat flux is the heat flow divided by the heat transfer surface area.
- Calculating a stream function as a function of depth and density provides a new way to analyze the thermodynamic character of ocean circulation. The sign of overturning cells in this stream function indicates whether cells are driven by wind stress or thermal forcing through heat conduction and mixing.
- The integral of the stream function gives the thermodynamic work performed by the fluid. This analysis approach is also valid for the Boussinesq equations, where formally there is no thermodynamic work in an incompressible fluid.
- The thermodynamic work in the Boussinesq equations appears as the generation of potential energy through heat conduction, and can be calculated as an integral of the stream function over depth and density.
There are three modes of convection heat transfer: forced convection, natural convection, and mixed convection. Forced convection occurs when fluid motion is generated by external forces like pumps or fans. Natural convection occurs when fluid motion is driven by gravity due to temperature gradients. Mixed convection occurs when external forces and gravitational forces are both present. The heat transfer coefficient depends on parameters like geometry, flow rate, flow conditions, and fluid type. It can range from around 10 W/m2°C for air in natural convection to over 100,000 W/m2°C for water in pool boiling.
A heat exchanger transfers energy between two or more fluids via a separating wall. Common configurations include counterflow, parallel tubes, cross-flow, and shell-and-tube designs. When applying an energy balance to a heat exchanger, kinetic and potential energy changes can be ignored, as well as heat transfer between the exchanger and surroundings. The balance simplifies to an equation relating the mass flow rates and enthalpy changes of the fluids. For a condenser example, assumptions allow the energy balance to drop certain terms and solve for the ratio of cooling water to steam mass flow rates.
This document provides an overview of chapter 5 of a thermodynamics textbook, which covers mass and energy analysis of control volumes. The key objectives are to develop the conservation of mass and first law of thermodynamics as applied to control volumes. It defines concepts like mass flow rate, volume flow rate, enthalpy, and flow work. Examples are provided to demonstrate applying conservation of mass to problems involving steady and unsteady flow systems as well as compressible and incompressible fluids. The chapter also discusses applying the energy balance to steady flow systems like nozzles, compressors, and heat exchangers.
The document summarizes a lab experiment that tested the efficiency of parallel and counter-flow heat exchangers. Equations were developed to calculate efficiency based on inlet and outlet temperatures and flow rates. The results showed that parallel flow had higher efficiency values than counter-flow, with efficiencies ranging from 22-56% for parallel flow and 4-13% for counter-flow. The higher efficiency of parallel flow was due to its larger temperature differences and faster mass flow rates.
Obtain average velocity from a knowledge of velocity profile, and average temperature from a knowledge of temperature profile in internal flow.
Have a visual understanding of different flow regions in internal flow, and calculate hydrodynamic and thermal entry lengths.
Analyze heating and cooling of a fluid flowing in a tube under constant surface temperature and constant surface heat flux conditions, and work with the logarithmic mean temperature difference.
Obtain analytic relations for the velocity profile, pressure drop, friction factor, and Nusselt number in fully developed laminar flow.
Determine the friction factor and Nusselt number in fully developed turbulent flow using empirical relations, and calculate the heat transfer rate.
This document discusses mass and energy analysis of control volumes for steady-flow engineering devices. It covers topics like nozzles, diffusers, turbines, compressors, throttling valves, mixing chambers, heat exchangers, and pipe/duct flow. Examples are provided for analyzing the energy and mass balances of these systems using the first law of thermodynamics. The document concludes with assigning homework problems involving these thermodynamic concepts.
Thermo problems (cascade refrigeration cycle ) mohammad usman
This document outlines a semester project for six students at Wah Engineering College, University of Wah. The project will cover topics including turbines, re-heaters, cascade refrigeration systems, and heat exchangers. It lists the group members and assumptions made. It also includes a sample problem solving a cascade refrigeration system, showing process points, temperatures, pressures, enthalpies and entropies. Questions are presented at the end for the students to answer as part of their project.
- Calculating a stream function as a function of depth and density provides a new way to analyze the thermodynamic character of ocean circulation. The sign of overturning cells in this stream function indicates whether cells are driven by wind stress or thermal forcing through heat conduction and mixing.
- The integral of the stream function gives the thermodynamic work performed by the fluid. This analysis approach is also valid for the Boussinesq equations, where formally there is no thermodynamic work in an incompressible fluid.
- The thermodynamic work in the Boussinesq equations appears as the generation of potential energy through heat conduction, and can be calculated as an integral of the stream function over depth and density.
There are three modes of convection heat transfer: forced convection, natural convection, and mixed convection. Forced convection occurs when fluid motion is generated by external forces like pumps or fans. Natural convection occurs when fluid motion is driven by gravity due to temperature gradients. Mixed convection occurs when external forces and gravitational forces are both present. The heat transfer coefficient depends on parameters like geometry, flow rate, flow conditions, and fluid type. It can range from around 10 W/m2°C for air in natural convection to over 100,000 W/m2°C for water in pool boiling.
A heat exchanger transfers energy between two or more fluids via a separating wall. Common configurations include counterflow, parallel tubes, cross-flow, and shell-and-tube designs. When applying an energy balance to a heat exchanger, kinetic and potential energy changes can be ignored, as well as heat transfer between the exchanger and surroundings. The balance simplifies to an equation relating the mass flow rates and enthalpy changes of the fluids. For a condenser example, assumptions allow the energy balance to drop certain terms and solve for the ratio of cooling water to steam mass flow rates.
This document provides an overview of chapter 5 of a thermodynamics textbook, which covers mass and energy analysis of control volumes. The key objectives are to develop the conservation of mass and first law of thermodynamics as applied to control volumes. It defines concepts like mass flow rate, volume flow rate, enthalpy, and flow work. Examples are provided to demonstrate applying conservation of mass to problems involving steady and unsteady flow systems as well as compressible and incompressible fluids. The chapter also discusses applying the energy balance to steady flow systems like nozzles, compressors, and heat exchangers.
The document summarizes a lab experiment that tested the efficiency of parallel and counter-flow heat exchangers. Equations were developed to calculate efficiency based on inlet and outlet temperatures and flow rates. The results showed that parallel flow had higher efficiency values than counter-flow, with efficiencies ranging from 22-56% for parallel flow and 4-13% for counter-flow. The higher efficiency of parallel flow was due to its larger temperature differences and faster mass flow rates.
Obtain average velocity from a knowledge of velocity profile, and average temperature from a knowledge of temperature profile in internal flow.
Have a visual understanding of different flow regions in internal flow, and calculate hydrodynamic and thermal entry lengths.
Analyze heating and cooling of a fluid flowing in a tube under constant surface temperature and constant surface heat flux conditions, and work with the logarithmic mean temperature difference.
Obtain analytic relations for the velocity profile, pressure drop, friction factor, and Nusselt number in fully developed laminar flow.
Determine the friction factor and Nusselt number in fully developed turbulent flow using empirical relations, and calculate the heat transfer rate.
This document discusses mass and energy analysis of control volumes for steady-flow engineering devices. It covers topics like nozzles, diffusers, turbines, compressors, throttling valves, mixing chambers, heat exchangers, and pipe/duct flow. Examples are provided for analyzing the energy and mass balances of these systems using the first law of thermodynamics. The document concludes with assigning homework problems involving these thermodynamic concepts.
Thermo problems (cascade refrigeration cycle ) mohammad usman
This document outlines a semester project for six students at Wah Engineering College, University of Wah. The project will cover topics including turbines, re-heaters, cascade refrigeration systems, and heat exchangers. It lists the group members and assumptions made. It also includes a sample problem solving a cascade refrigeration system, showing process points, temperatures, pressures, enthalpies and entropies. Questions are presented at the end for the students to answer as part of their project.
This document describes a laboratory experiment conducted by chemical engineering students at Polytechnic University of Puerto Rico to analyze heat transfer in a shell and tube heat exchanger. The objectives were to determine the overall heat transfer coefficient using the logarithmic mean temperature difference method and calculate efficiency at different flowrates in co-current and counter-current configurations. Temperature and flowrate data was collected and used to calculate efficiencies, heat transfer coefficients, and investigate the effects of flowrate and direction on heat transfer performance. Safety procedures were followed to properly conduct the experiment.
two dimensional steady state heat conduction Amare Addis
This document provides information about two-dimensional steady state heat conduction using the finite difference method. It includes:
1) Derivation of the finite difference equations for interior nodes, nodes on insulated surfaces, and nodes with convection boundary conditions using the energy balance method.
2) Discussion of using shape factors and dimensionless parameters to simplify solving two-dimensional conduction problems.
3) Methods for verifying the accuracy of finite difference solutions, including grid refinement studies and comparison to exact solutions.
This document discusses methods for solving fluid flow problems. It outlines two essential equations: [1] the equation of continuity, which states that the inflow equals the outflow in steady flow through a control volume, and [2] the Bernoulli equation, which relates pressure, velocity, and elevation along a streamline based on the principle of conservation of energy. Common applications where these equations are used include pipes, rivers, and overall processes. The procedure for solving flow problems involves choosing a datum plane, noting where velocity, pressure, and other variables are known or to be assumed, and applying the continuity and Bernoulli equations.
The document discusses heat transfer fins, which are solid extensions that increase heat transfer between a solid surface and surrounding fluid. Fins transfer heat through conduction within themselves and convection at their surfaces. They are used when heat transfer coefficients are small to increase the surface area and thus the rate of heat dissipation. Common applications include radiators, motor casings, and heat exchangers. The document provides equations to model fin heat transfer and discusses fin materials, shapes, and the difference between fin effectiveness and efficiency.
In this A 2D Navier-stokes equation is used to study steady state laminar flow over a backward facing step for dimension less duct. The Reynolds number used for this flow is Re=Uh/ν where Reh=229 for Denham and Patrick and Reh=178 and 233 for Aung’s Experiment. i.e. The results obtained are then compared using the excel software for which the data of Velocity profile and Reattachment length for the temperature profile in both recirculating and non-recirculating zone by using Para view. (Salome 8.3.0, sim flow)
Recognize numerous types of heat exchangers, and classify them.
Develop an awareness of fouling on surfaces, and determine the overall heat transfer coefficient for a heat exchanger.
Perform a general energy analysis on heat exchangers.
Obtain a relation for the logarithmic mean temperature difference for use in the LMTD method, and modify it for different types of heat exchangers using the correction factor.
Develop relations for effectiveness, and analyze heat exchangers when outlet temperatures are not known using the effectiveness-NTU method.
Know the primary considerations in the selection of heat exchangers.
This document discusses heat transfer through extended surfaces called fins. It begins by introducing fins and explaining that they are used to increase the surface area for heat transfer. It then derives the governing differential equation for one-dimensional, steady-state heat conduction through a fin. The document explores several boundary conditions and derives equations for the temperature distribution, heat transfer rate, and efficiency of fins with different boundary conditions, including infinitely long fins, fins with an insulated tip, and fins with a prescribed tip temperature. It concludes by discussing fin effectiveness and the factors that influence it.
Heat transfer from extended surfaces (or fins)tmuliya
This file contains slides on Heat Transfer from Extended Surfaces (FINS). The slides were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India.
Contents: Governing differential eqn – different boundary conditions – temp. distribution and heat transfer rate for: infinitely long fin, fin with insulated end, fin losing heat from its end, and fin with specified temperatures at its ends – performance of fins - ‘fin efficiency’ and ‘fin effectiveness’ – fins of non-uniform cross-section- thermal resistance and total surface efficiency of fins – estimation of error in temperature measurement - Problems
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTSsureshkcet
This document discusses gas dynamics and jet propulsion. It covers fundamental concepts of compressible flow, including the energy and momentum equations. It also discusses isentropic flow through variable area ducts like nozzles and diffusers. The conservation of mass, momentum and energy are applied to one-dimensional, steady, inviscid flow. The flow is analyzed through a variable area duct and expressions are developed relating pressure, velocity, temperature and Mach number for a perfect gas. Frictional flow in a constant area duct is also analyzed.
The document presents a linear programming formulation to minimize utility costs for a heat exchanger network. Hot and cold streams are available along with utility options like fuel, high pressure steam, and low pressure steam. The goal is to predict costs while meeting a minimum 10K approach and not allowing stream H1 to exchange heat with stream C1. The problem is modeled as a transshipment problem and formulated as a linear program to find the optimal heat exchange between streams and utilities. The solution found using GAMS software indicates a minimum utility cost of $570,000 per year can be achieved while meeting the constraints.
The document analyzes heat transfer in the hot gas path of a gas turbine for a semi-closed oxy-combustion combined cycle (SCOC-CC) power plant under different operating conditions. It evaluates the convective and radiative heat transfer to the first row turbine vane using empirical correlations. The analysis shows that SCOC-CC with flue gas recirculation before condensation results in 20-30% higher heat transfer compared to recirculation after condensation. Increasing the pressure ratio from 17 to 40 at constant thermal power and turbine inlet temperature increases both convective and radiative heat transfer by about 10%. Chemiluminescence is found to have a negligible effect on heat transfer as the
This document outlines key concepts in gas dynamics and compressible flow. It defines gas dynamics as the branch of fluid dynamics concerned with compressible flow. Some main topics covered include the fundamental laws of thermodynamics, definitions of basic terms like system and state, and equations for the conservation of mass, momentum and energy. It also discusses different types of flow and processes like steady/unsteady, laminar/turbulent and adiabatic. Stagnation properties of gases are defined using equations relating stagnation temperature, pressure and density to static properties.
Why do I Need SURFsara Cloud Facility in My Research?Ali Abbasi
This document discusses why researchers may need access to SURFsara Cloud Facility for their work estimating evaporation from water surfaces. It describes using computational fluid dynamics (CFD) to simulate both the water body and atmospheric boundary layer, which requires significant computing power. Parallel computing is necessary to run the models efficiently, decomposing the tasks across multiple processors. While some computing could be done on a local PC or shared cluster, the SURFsara HPC-Cloud provides additional computational resources well-suited for such large-scale simulations.
Numerical Study of Forced Convection in a Rectangular Channel
Original Research Article
Journal of Chemistry and Materials Research Vol. 1 (1), 2014, 7–11
Salim Gareh
This document discusses energy analysis of closed systems, including specific heats at constant volume and pressure, internal energy, enthalpy, and specific heats of ideal gases and incompressible substances like solids and liquids. It provides equations relating these concepts and explains how to calculate changes in internal energy and enthalpy using data tables, functional forms of specific heats, or average specific heat values. Examples are also included.
This document summarizes a presentation for a Master's degree in mechanical engineering. It simulates steam flow in a rectangular duct using governing equations to model the velocity and temperature profiles. The simulation shows the developing velocity profile within the duct and temperature distribution outside as the steam heats the surroundings. Results demonstrate the velocity is highest in the duct's center and drops towards the edges, forming a boundary layer. The temperature graphs also show the surroundings reaching a steady state of heat transfer within 1 second of introducing the steam.
One dim, steady-state, heat conduction_with_heat_generationtmuliya
This file contains slides on One-dimensional, steady-state heat conduction with heat generation.
The slides were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India, during Sept. – Dec. 2010.
It is hoped that these Slides will be useful to teachers, students, researchers and professionals working in this field.
This file contains slides on Transient Heat conduction: Part-II
The slides were prepared while teaching Heat Transfer course to the M.Tech. students in the year 2010.
Contents: Semi-infinite solids with different BC’s - Problems - Product solution for multi-dimension systems -
Summary of Basic relations for transient conduction
1) The document presents the analysis of heat transfer through a triangular fin using finite difference methods. Temperature profiles were calculated at 8 nodes along the fin using energy balance equations and a numerical solution in Mathcad.
2) The temperatures decrease along the fin from 115°C at the base to 31.55°C at the tip. The effectiveness of the fin is 2.58 and efficiency is 50.5%.
3) The total heat flow rate at the base is 824.807 W, which is equal to the sum of the convective heat transfer rates calculated at each node.
Mathcad Functions for Conduction heat transfer calculationstmuliya
This file contains notes on Mathcad Functions for Conduction heat transfer calculations. Some problems are also included.
These notes were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India.
It is hoped that these notes will be useful to teachers, students, researchers and professionals working in this field.
This document describes a laboratory experiment conducted by chemical engineering students at Polytechnic University of Puerto Rico to analyze heat transfer in a shell and tube heat exchanger. The objectives were to determine the overall heat transfer coefficient using the logarithmic mean temperature difference method and calculate efficiency at different flowrates in co-current and counter-current configurations. Temperature and flowrate data was collected and used to calculate efficiencies, heat transfer coefficients, and investigate the effects of flowrate and direction on heat transfer performance. Safety procedures were followed to properly conduct the experiment.
two dimensional steady state heat conduction Amare Addis
This document provides information about two-dimensional steady state heat conduction using the finite difference method. It includes:
1) Derivation of the finite difference equations for interior nodes, nodes on insulated surfaces, and nodes with convection boundary conditions using the energy balance method.
2) Discussion of using shape factors and dimensionless parameters to simplify solving two-dimensional conduction problems.
3) Methods for verifying the accuracy of finite difference solutions, including grid refinement studies and comparison to exact solutions.
This document discusses methods for solving fluid flow problems. It outlines two essential equations: [1] the equation of continuity, which states that the inflow equals the outflow in steady flow through a control volume, and [2] the Bernoulli equation, which relates pressure, velocity, and elevation along a streamline based on the principle of conservation of energy. Common applications where these equations are used include pipes, rivers, and overall processes. The procedure for solving flow problems involves choosing a datum plane, noting where velocity, pressure, and other variables are known or to be assumed, and applying the continuity and Bernoulli equations.
The document discusses heat transfer fins, which are solid extensions that increase heat transfer between a solid surface and surrounding fluid. Fins transfer heat through conduction within themselves and convection at their surfaces. They are used when heat transfer coefficients are small to increase the surface area and thus the rate of heat dissipation. Common applications include radiators, motor casings, and heat exchangers. The document provides equations to model fin heat transfer and discusses fin materials, shapes, and the difference between fin effectiveness and efficiency.
In this A 2D Navier-stokes equation is used to study steady state laminar flow over a backward facing step for dimension less duct. The Reynolds number used for this flow is Re=Uh/ν where Reh=229 for Denham and Patrick and Reh=178 and 233 for Aung’s Experiment. i.e. The results obtained are then compared using the excel software for which the data of Velocity profile and Reattachment length for the temperature profile in both recirculating and non-recirculating zone by using Para view. (Salome 8.3.0, sim flow)
Recognize numerous types of heat exchangers, and classify them.
Develop an awareness of fouling on surfaces, and determine the overall heat transfer coefficient for a heat exchanger.
Perform a general energy analysis on heat exchangers.
Obtain a relation for the logarithmic mean temperature difference for use in the LMTD method, and modify it for different types of heat exchangers using the correction factor.
Develop relations for effectiveness, and analyze heat exchangers when outlet temperatures are not known using the effectiveness-NTU method.
Know the primary considerations in the selection of heat exchangers.
This document discusses heat transfer through extended surfaces called fins. It begins by introducing fins and explaining that they are used to increase the surface area for heat transfer. It then derives the governing differential equation for one-dimensional, steady-state heat conduction through a fin. The document explores several boundary conditions and derives equations for the temperature distribution, heat transfer rate, and efficiency of fins with different boundary conditions, including infinitely long fins, fins with an insulated tip, and fins with a prescribed tip temperature. It concludes by discussing fin effectiveness and the factors that influence it.
Heat transfer from extended surfaces (or fins)tmuliya
This file contains slides on Heat Transfer from Extended Surfaces (FINS). The slides were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India.
Contents: Governing differential eqn – different boundary conditions – temp. distribution and heat transfer rate for: infinitely long fin, fin with insulated end, fin losing heat from its end, and fin with specified temperatures at its ends – performance of fins - ‘fin efficiency’ and ‘fin effectiveness’ – fins of non-uniform cross-section- thermal resistance and total surface efficiency of fins – estimation of error in temperature measurement - Problems
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTSsureshkcet
This document discusses gas dynamics and jet propulsion. It covers fundamental concepts of compressible flow, including the energy and momentum equations. It also discusses isentropic flow through variable area ducts like nozzles and diffusers. The conservation of mass, momentum and energy are applied to one-dimensional, steady, inviscid flow. The flow is analyzed through a variable area duct and expressions are developed relating pressure, velocity, temperature and Mach number for a perfect gas. Frictional flow in a constant area duct is also analyzed.
The document presents a linear programming formulation to minimize utility costs for a heat exchanger network. Hot and cold streams are available along with utility options like fuel, high pressure steam, and low pressure steam. The goal is to predict costs while meeting a minimum 10K approach and not allowing stream H1 to exchange heat with stream C1. The problem is modeled as a transshipment problem and formulated as a linear program to find the optimal heat exchange between streams and utilities. The solution found using GAMS software indicates a minimum utility cost of $570,000 per year can be achieved while meeting the constraints.
The document analyzes heat transfer in the hot gas path of a gas turbine for a semi-closed oxy-combustion combined cycle (SCOC-CC) power plant under different operating conditions. It evaluates the convective and radiative heat transfer to the first row turbine vane using empirical correlations. The analysis shows that SCOC-CC with flue gas recirculation before condensation results in 20-30% higher heat transfer compared to recirculation after condensation. Increasing the pressure ratio from 17 to 40 at constant thermal power and turbine inlet temperature increases both convective and radiative heat transfer by about 10%. Chemiluminescence is found to have a negligible effect on heat transfer as the
This document outlines key concepts in gas dynamics and compressible flow. It defines gas dynamics as the branch of fluid dynamics concerned with compressible flow. Some main topics covered include the fundamental laws of thermodynamics, definitions of basic terms like system and state, and equations for the conservation of mass, momentum and energy. It also discusses different types of flow and processes like steady/unsteady, laminar/turbulent and adiabatic. Stagnation properties of gases are defined using equations relating stagnation temperature, pressure and density to static properties.
Why do I Need SURFsara Cloud Facility in My Research?Ali Abbasi
This document discusses why researchers may need access to SURFsara Cloud Facility for their work estimating evaporation from water surfaces. It describes using computational fluid dynamics (CFD) to simulate both the water body and atmospheric boundary layer, which requires significant computing power. Parallel computing is necessary to run the models efficiently, decomposing the tasks across multiple processors. While some computing could be done on a local PC or shared cluster, the SURFsara HPC-Cloud provides additional computational resources well-suited for such large-scale simulations.
Numerical Study of Forced Convection in a Rectangular Channel
Original Research Article
Journal of Chemistry and Materials Research Vol. 1 (1), 2014, 7–11
Salim Gareh
This document discusses energy analysis of closed systems, including specific heats at constant volume and pressure, internal energy, enthalpy, and specific heats of ideal gases and incompressible substances like solids and liquids. It provides equations relating these concepts and explains how to calculate changes in internal energy and enthalpy using data tables, functional forms of specific heats, or average specific heat values. Examples are also included.
This document summarizes a presentation for a Master's degree in mechanical engineering. It simulates steam flow in a rectangular duct using governing equations to model the velocity and temperature profiles. The simulation shows the developing velocity profile within the duct and temperature distribution outside as the steam heats the surroundings. Results demonstrate the velocity is highest in the duct's center and drops towards the edges, forming a boundary layer. The temperature graphs also show the surroundings reaching a steady state of heat transfer within 1 second of introducing the steam.
One dim, steady-state, heat conduction_with_heat_generationtmuliya
This file contains slides on One-dimensional, steady-state heat conduction with heat generation.
The slides were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India, during Sept. – Dec. 2010.
It is hoped that these Slides will be useful to teachers, students, researchers and professionals working in this field.
This file contains slides on Transient Heat conduction: Part-II
The slides were prepared while teaching Heat Transfer course to the M.Tech. students in the year 2010.
Contents: Semi-infinite solids with different BC’s - Problems - Product solution for multi-dimension systems -
Summary of Basic relations for transient conduction
1) The document presents the analysis of heat transfer through a triangular fin using finite difference methods. Temperature profiles were calculated at 8 nodes along the fin using energy balance equations and a numerical solution in Mathcad.
2) The temperatures decrease along the fin from 115°C at the base to 31.55°C at the tip. The effectiveness of the fin is 2.58 and efficiency is 50.5%.
3) The total heat flow rate at the base is 824.807 W, which is equal to the sum of the convective heat transfer rates calculated at each node.
Mathcad Functions for Conduction heat transfer calculationstmuliya
This file contains notes on Mathcad Functions for Conduction heat transfer calculations. Some problems are also included.
These notes were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India.
It is hoped that these notes will be useful to teachers, students, researchers and professionals working in this field.
Mathcad Functions for Forced convection heat transfer calculationstmuliya
This file contains notes on Mathcad Functions for Forced convection heat transfer calculations. Some problems are also included.
These notes were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India. It is hoped that these notes will be useful to teachers, students, researchers and professionals working in this field.
Contents: Forced convection formulas – boundary layer, flow over flat plates, across cylinders, spheres and tube banks
Mathcad Functions for Natural (or free) convection heat transfer calculationstmuliya
This file contains notes on Mathcad Functions for Natural (or, free) convection heat transfer calculations. Some problems are also included.
These notes were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India.
It is hoped that these notes will be useful to teachers, students, researchers and professionals working in this field.
Contents: Free convection from vertical plates and cylinders, horizontal plates, cylinders and spheres, enclosed spaces, rotating cylinders, disks and spheres. Finned surfaces.
Combined Natural and Forced convection.
Math cad effective radiation heat transfer coefficient.xmcdJulio Banks
The document discusses the effective radiation heat transfer coefficient (hr) and provides an example calculation. It defines hr as the "radiation heat transfer coefficient" and gives the equation for calculating hr based on the emissivities and absolute temperatures of two surfaces. The example calculates hr for a heated cylindrical rod in a vacuum furnace, finding the heat flux and total heat transfer rate based on the surface area and temperature difference. A plot is provided showing how hr varies with the sink temperature.
This document discusses the simulation of a missile's surface temperature over time. It provides governing equations that model the temperature change based on convection from the surrounding air and thermal radiation. Parameters like the missile's velocity, ambient air properties at different altitudes, and the missile's material properties are defined. The equations are solved numerically over a 10 second period to generate a temperature history profile for the missile's skin.
MathCAD FEA vallidation by caefem of capped-cylinder stressesJulio Banks
This document presents a closed-form analysis and finite element analysis of stresses in a cylindrical shell connected to a circular plate under internal pressure. It provides equations and calculations for geometry, material properties, stress components, and von Mises stress at the junction. The closed-form von Mises stress of 13.78 ksi compares favorably with the finite element analysis result of 14.20 ksi, with a difference of 3.1%. This validation demonstrates that closed-form solutions can be used to check finite element analysis results for relatively simple configurations.
NUMERICAL METHODS IN STEADY STATE, 1D and 2D HEAT CONDUCTION- Part-IItmuliya
This document discusses numerical methods for solving steady-state 1D and 2D heat conduction problems. It describes the relaxation method, Gaussian elimination method, and Gauss-Siedel iteration method for solving systems of simultaneous algebraic equations arising in heat conduction analyses. The Gaussian elimination and matrix inversion methods use matrix operations to systematically eliminate variables. The Gauss-Siedel iteration method iteratively solves for each variable using the most recently calculated values of other variables until convergence is reached. Examples are provided to illustrate each numerical solution technique.
Mathcad functions for fluid properties - for convection heat transfer calcu...tmuliya
This file contains slides on Mathcad Functions for Fluid properties--- Useful in Convection heat transfer calculations.
The slides were prepared while teaching Heat Transfer course to the M.Tech. students in Mechanical Engineering Dept. of St. Joseph Engineering College, Vamanjoor, Mangalore, India, during Sept. – Dec. 2010.
It is hoped that these Slides will be useful to teachers, students, researchers and professionals working in this field.
Contents: Mathcad Functions for properties of:
Air, Ammonia, Ethyl alcohol, Ethylene glycol, Un-used engine oil, Glycerin, Lead, and Mercury
PTC Mathcad Prime 4.0 is an engineering math software that allows users to securely perform and share calculations. It offers content protection to control access and visibility of intellectual property, interoperability with third-party applications like MS Word, improved usability through equation wrapping, and management of large worksheets. The software calculates results while communicating designs through plots, graphs, text, and images in a single document.
Tracxn Research - Construction Tech Landscape, February 2017Tracxn
The document provides an overview of investment trends in the construction technology sector from 2008 to 2016. It finds that the number of startups founded and funding rounds increased year over year, with total funding reaching $491 million in 2016. Early stage funding amounts and average ticket sizes also increased over time, with average early stage deals reaching $11.9 million in 2016. The report also analyzes subsectors of construction tech and provides examples of interesting startups.
1. The document discusses heat transfer from extended surfaces, or fins, which are structures that enhance heat transfer between a solid surface and surrounding fluid.
2. A general conduction analysis is presented to determine the temperature distribution along a fin by applying an energy balance to differential elements.
3. Specific solutions are obtained for fins of uniform cross-sectional area, considering different boundary conditions at the fin tip, including convection, an insulated tip, and a prescribed temperature. Expressions are derived for the temperature distribution and heat transfer rate from the fin.
Convective heat transfer and pressure drop in v corrugatedMohamed Fadl
New energy system development and energy
conservation require high performance heat exchanger, so
the researchers are seeking to find new methods to enhance
heat transfer mechanism in heat exchangers. The objectives
of this study are investigating heat transfer performance
and flow development in V-corrugated channels, numerical
simulations were carried out for uniform wall heat flux
equal 290 W/m
2
using air as a working fluid, Reynolds
number varies from 500 to 2,000, phase shifts,
0 \ Ø \ 180, and channel heights (S = 12.5, 15.0, 17.5
and 20 mm). Governing equations of flow and energy were
solved numerically by using finite volume method. The
numerical results indicated that, wavy (V-corrugated)
channels have a significant impact on heat transfer
enhancement with increase in pressure drop though chan-
nel due to breaking and destabilizing in the thermal
boundary layer are occurred as fluid flowing through the
corrugated surfaces and the effect of corrugated phase shift
on the heat transfer and fluid flow is more significant in
narrow channel, the goodness factor (j/f) was increased
with increasing channel phase shift, the best performance
was noticed on phase shift, Ø = 180 and channel height,
S = 12.5 mm.
This document discusses heat exchangers and includes the following key points:
- It describes different types of heat exchangers including concentric-tube, cross-flow, shell-and-tube, and compact heat exchangers.
- It discusses the overall heat transfer coefficient and factors that influence it such as convection, conduction, fins, and fouling.
- It introduces the log mean temperature difference (LMTD) method for calculating heat transfer in heat exchangers and how LMTD is evaluated for different flow configurations.
- It provides an example problem demonstrating how to determine the overall heat transfer coefficient and heat transfer rate for a heat recovery device.
This document discusses heat exchangers, including their types, performance parameters, and design methodologies. It introduces the log mean temperature difference method for relating heat transfer rate to inlet/outlet temperatures. It also describes the effectiveness-NTU method, where effectiveness is defined as the ratio of actual to maximum possible heat transfer, and NTU is the number of transfer units. Sample problems demonstrate the use of these methods to determine required surface areas, heat transfer rates, and outlet temperatures for given heat exchanger configurations and operating conditions.
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1) The document discusses heat transfer by conduction through plane walls and cylindrical pipes. It presents the general heat conduction equations and derives the equations for the temperature distribution in plane walls and cylindrical pipes.
2) It also discusses heat transfer by convection and defines the overall heat transfer coefficient (U) for a plane wall subjected to convection on both sides. Expressions are developed for the surface temperatures and overall heat transfer coefficient.
3) An example problem is presented to calculate the surface temperatures and overall heat transfer coefficient for a plane wall subjected to a uniform heat flux on one side and convection on the other.
lecture pf control system_thermal system_206.pdfAtmacaDevrim
The document discusses thermal systems and concepts such as:
- Thermal systems involve the storage and transfer of energy as heat. Heat flows from higher to lower temperatures.
- The law of conservation of energy applies to thermal systems, where the change in internal energy equals heat supplied minus work done.
- Thermal resistance and capacitance relate temperature differences and heat flow in thermal systems, analogous to voltage and capacitance in electrical systems.
- Heat transfer occurs through conduction, convection and radiation, and can be modeled using concepts like Newton's law of cooling.
The document summarizes key concepts of heat transfer including the three main modes: conduction, convection, and radiation. It provides equations to calculate heat transfer via these three modes. Specifically, it discusses Fourier's law of conduction, Newton's law of cooling for convection, and Stefan-Boltzmann law for radiation heat transfer. It also introduces important non-dimensional numbers used in heat transfer such as Reynolds number, Prandtl number, Nusselt number, and Stanton number.
- Any reversible process can be approximated by a series of reversible, isothermal and reversible, adiabatic processes connected by intermediate states.
- The heat interaction along the reversible path is equal to the heat interaction along the reversible isothermal path between the same initial and final states.
- Therefore, a reversible process can be replaced by a zig-zag path consisting of reversible adiabatic and isothermal processes, satisfying the first law of thermodynamics.
- According to the Clausius theorem, the integral of heat transfer divided by temperature around any cyclic process is equal to zero for a reversible process. This leads to the definition of entropy as a state function.
Numerical Analysis of heat transfer in a channel Wit in clined bafflesinventy
Research Inventy : International Journal of Engineering and Science is published by the group of young academic and industrial researchers with 12 Issues per year. It is an online as well as print version open access journal that provides rapid publication (monthly) of articles in all areas of the subject such as: civil, mechanical, chemical, electronic and computer engineering as well as production and information technology. The Journal welcomes the submission of manuscripts that meet the general criteria of significance and scientific excellence. Papers will be published by rapid process within 20 days after acceptance and peer review process takes only 7 days. All articles published in Research Inventy will be peer-reviewed.
GATE Mechanical Engineering notes on Heat Transfer. Use these notes as a preparation for GATE Mechanical Engineering and other engineering competitive exams. For full course visit https://mindvis.in/courses/gate-2018-mechanical-engineering-online-course or call 9779434433.
This document provides an introduction to heat transfer and the different modes of heat transfer including conduction, convection, radiation, boiling, and condensation. It defines key terms like thermal conductivity and heat flux. Examples of one-dimensional heat conduction through plane walls, cylindrical walls, and multilayer walls are presented. The document also provides sample problems and their solutions for determining heat transfer rates through composite walls and insulated cylinders.
Energy transfer by heat occurs between systems with a temperature difference, even if no work is done. Heat transfer is driven by decreasing temperature, with a higher rate of transfer for larger temperature differences. Heat transfer between a system and its surroundings is represented by Q, with a positive Q indicating heat transfer to the system. For transient processes, the rate of energy transfer to or from a system can be determined by integrating heat (Q) and work (W) terms over time.
Heat Conduction with thermal heat generation.pptxBektu Dida
Heat Conduction analysis is done in one dimensional steady state heat conduction considering internal heat generation per unit volume on plane and radial walls. Examples are directly taken from textbooks.
1. The document discusses energy balances for chemical reactors, deriving equations to determine reactor temperature based on heat and work terms.
2. Special cases are considered, including constant pressure/volume reactors and incompressible fluids. Equations are presented for batch reactors under these conditions.
3. A example problem compares constant pressure and volume reactors for an irreversible decomposition reaction, showing the constant volume reactor proceeds faster due to less work required.
Basic heat exchanger equations and calculations outlines three key equations for calculating the rate of heat exchange (Q) in an adiabatic heat exchanger with no heat loss to the environment. The equations relate Q to the mass flow rates, specific enthalpies, and temperatures of the process and utility streams. HYSYS software uses the first equation to calculate Q for heaters/coolers and heat exchangers based on specifications for two streams. It displays Q/average temperature difference as the overall heat transfer coefficient (U) times the heat transfer area (A), which must be divided by U and a correction factor F to determine the actual heat exchanger area A.
This tutorial covers heat transfer via convection and radiation. It discusses:
- Natural and forced convection, and how to calculate heat transfer rates using surface heat transfer coefficients.
- Combining conduction and convection to solve problems involving multi-layer surfaces.
- The basic theory of radiated heat transfer, and how emissivity and surface shape affect heat transfer rates.
- Calculating effective surface heat transfer coefficients to model radiation using similar equations as convection.
- Worked examples are provided to demonstrate calculating heat transfer rates via combined conduction, convection and radiation in practical scenarios.
This document provides an overview of heat and mass transfer. It defines heat and mass transfer as dealing with the rate of transfer of thermal energy and discusses the three main modes of heat transfer: conduction, convection, and radiation. It also outlines some key topics that will be covered, including Fourier's law of conduction, Newton's law of cooling, Stefan-Boltzmann's law of radiation, thermal conductivity, heat transfer in gases, and heat exchangers. Equations for one-dimensional and radial conduction are presented.
This document discusses heat exchangers and provides details on shell-and-tube heat exchangers. It describes the basic components and design of shell-and-tube heat exchangers, including tubes, tube sheets, baffles, and shells. Equations for heat transfer and thermal analysis of shell-and-tube exchangers are presented. An example problem demonstrates the design calculations to determine the required heat exchanger area and fluid flow rates.
The document discusses the second law of thermodynamics and various reversible processes on a temperature-entropy (T-s) diagram for a perfect gas. It defines:
1) Constant pressure, volume, temperature, adiabatic, and polytropic processes on a T-s diagram.
2) Equations to calculate work, heat, and entropy change for constant pressure, volume, and temperature processes.
3) Provides an example problem calculating properties of air undergoing two processes - constant volume heating and constant pressure cooling.
Similar to Math cad advection-convection heat transfer (20)
Apologia - A Call for a Reformation of Christian Protestants Organizations.pdfJulio Banks
This document shows how to know whether an organization claiming to be IRS 501(C)(3) tax exempted nonprofit is being partisan by teaching that the republican party is the party of Jesus Christ violating the nonpartisan IRS requirement are false Christian organizations.
The treatment of large structural systems may be simplified by dividing the system into
smaller systems called components. The components are related through the
displacement, and force conditions at their junction points. Each component is represented
by mode shapes (or functions).
The document describes an algorithm to determine the common or synchronization period (Tc) of two independent asynchronous events with periods of ta and tb. The algorithm involves 4 steps: 1) Determine the maximum (t2) and minimum (t1) periods. 2) Calculate the difference in periods (Δt). 3) Determine the number of t2 periods in Δt (N2). 4) The synchronization period is Tc = N2 * t1. Two examples applying the algorithm are also provided.
This document provides guidance for Christians on how to effectively share the gospel with Muslims. It emphasizes unfolding God's word sequentially to show his panoramic rescue plan fulfilled in Jesus. Key points include: discussing eternity planted in the human heart and God's power to save as common ground; using Old Testament stories and quotes like Ecclesiastes 3:11-12 that resonate with Muslims; and following Jesus' gracious example in John 4 of conversing in a seasoned, question-answering way that led villagers to acknowledge him as Savior. The goal is engaging Muslims through meaningful conversation that traces the Bible's rescue themes.
Math cad prime the relationship between the cubit, meter, pi and the golden...Julio Banks
It has been reported that the ancient Egyptians knew pi, the golden ration (phi) and the meter. This paper summarizes the relationship of pi, and phi via the cubit.
Transcript for abraham_lincoln_thanksgiving_proclamation_1863Julio Banks
Lincoln's 1863 Thanksgiving Proclamation designated the last Thursday of November as a national day of Thanksgiving. It recognized the blessings of abundant harvests despite the ravages of the ongoing Civil War. Lincoln acknowledged that peace had been maintained with other nations and order and law had prevailed across most of the country, except for battlefields, where advancing Union armies had reduced areas of conflict. He attributed the nation's continued prosperity and population growth, despite wartime losses, to God's gracious gifts and providence. Lincoln called on citizens to offer gratitude and also humble prayers for healing of the nation and restoration of peace.
Thanksgiving and lincolns calls to prayerJulio Banks
1) Abraham Lincoln issued proclamations for national days of fasting, prayer, and thanksgiving during the Civil War, recognizing America's dependence on God for blessings and calling the nation to humble itself before God.
2) Lincoln prayed for victory at Gettysburg and vowed to stand for God if given victory, which may have turned the tide of the war.
3) After the war ended, Lincoln gathered his cabinet to thank God on their knees that the war was over, setting an example for the nation to acknowledge God's role in their blessings and salvation.
Jannaf 10 1986 paper by julio c. banks, et. al.-ballistic performance of lpg ...Julio Banks
This paper is the result of the response of LPG (Liquid Propellant Gun) to high-temperate simulated-desert condition using ANSYS FEA (Finite Element Analysis) and Mica Heating Banks.
web site: http://www.joycenter.net/wp-content/uploads/2013/04/Mans-Search-for-Meaning-Viktor-Frankl.pdf
A case can be made that since the main basis of "The Theory" of evolution is the "Self-preservation principle". That is, how could the propagation of the a specie be enhanced by the demeaning action of a group against its constituents and even self-against-self. The only explanation is that humas were created and not a result of a random sett of actions causing consciousness arriving from non-conscious matter. Life comes from life, and intelligence (DNA), comes from intelligence. This book can be contrasted with: The Lucifer Effect Understanding How Good People Turn Evil by Philip Zimbardo' and also with the Bible for a view of The Meaning of Life from ancient to contemporary writings for balance understanding of the physical (Psyche) to the metaphysical (Spiritual). We can view the human condition as the effect of gravity of interacting physical objects and human interaction as the response to spiritual influence (angels and demons).
The document discusses the concept of "shadow-self", which refers to humans projecting negative aspects of themselves onto others. It argues that true love and self-acceptance are the answers to overcoming this tendency. It provides several biblical passages about love and discusses how Jesus taught about being free from condemnation. The document concludes that psychological projection arises from psychological dissonance, and that finding one's "true self" through love and embracing uniqueness can lead to enlightenment.
The first step required to defeating an enemy is by first thoroughly defining it. A physician runs tests of their patients to determine the type of pathogen ailing such patients. Similarly, we must be clear that A Muslim Terrorist is indeed a Fundamentalist and not a Radical Terrorist since the method of striking terror is explicitly and clearly defined in the Qur'an. Christianity is the only religion that needs not attack any other religion such as the Islam religion since God is the author and finisher of our faith and also commands the Christians to allow God to avenge Himself for our attacks even from Islamic Terrorist. A Christian is commanded to live at peace with all humans and when such a peaceful coexistence is not achieved then we must simply stay away from such toxic humans.
The primary test for a true religion is that "The Judeo-Christian God does not need nor require that mere mortal human beings to defend Him".
NASA-TM-X-74335 --U.S. Standard Atmosphere 1976Julio Banks
NASA-TM-X-74335 --U.S. Standard Atmosphere 1976. This information is useful for airframes (e.g., missiles and aircrafts) aero-thermos analysis and design.
Mathcad P-elements linear versus nonlinear stress 2014-t6Julio Banks
This work couples the classical ESED (Equivalent Strain Energy Density) Method; aka, Glinka. The most expedient method of solving a structural problem using FEA (Finite Element Analysis). There would be occasions when stress concentrations would be calculated due to interior corners, holes, sudden change of geometry (aka stress raisers). Although some software would allow regions in the vicinity of such stress risers to be defined by nonlinear material models such as "Elastic Perfectly-plastic", "Bilinear (Elastic and linear plastic), or the fundamental Ramberg-Osgood metal strain-stress models. Once the Linear-elastic FEA solution is obtained one can readily determine that Pseduo nonlinear strain, the corresponding stress and the implicit stress-intensification factor, Kt. It should be noted that once the analyst-designer is ready for final analysis, it would be most prudent to create a FEA model in which the regions of high concentration of stress to be modeled with local nonlinear models of the metal using St. Vennants' Principle of load-and-resistance distance from area of interest. The P-method is an excellent FEA element that can "find the actual nonlinear stress" by the simple iterative increase of the order of the polynomial representing the stress fields within every P-element. It should be noted that this research was facilitated by the use of the P-element FEA software called StressCheck which is 100% P-element solution which I am quite pleased to have had the opportunity of utilizing for this research.
Apologia - The martyrs killed for clarifying the bibleJulio Banks
I know all the things you do, that you are neither hot nor cold. I wish that you were one or the other! 16But since you are like lukewarm water, neither hot nor cold, I will spit you out of my mouth!” - Revelation 3:15-16
“A man who does not have something for which he is willing to die is not fit to live.” - Martin Luther King Jr.
Apologia - Always be prepared to give a reason for the hope that is within yo...Julio Banks
1) Christians should be humble, compassionate, and unified in their love for one another, even in the face of suffering for doing good.
2) When suffering, Christians should bless those who harm them and not repay evil with evil.
3) The passage encourages Christians to always be prepared to explain the hope they have in Jesus Christ when asked, but to do so gently and respectfully.
Spontaneous creation of the universe ex nihil by maya lincoln and avi wasserJulio Banks
Questions regarding the formation of the Universe and ‘what was there ’ before it came to existence have
been of great interest to mankind at all times. Several suggestions have been presented during the ages –
mostly assuming a preliminary state prior to creation. Nevertheless, theories that require initial conditions
are not considered complete, since they lack an explanation of what created such conditions. We therefore
propose the ‘Creatio Ex Nihilo ’ (CEN) theory, aimed at describing the origin of the Universe from ‘nothing ’ in
information terms. The suggested framework does not require amendments to the laws of physics: but rather
provides a new scenario to the Universe initiation process, and from that point merges with state-of-the-art
cosmological models. The paper is aimed at providing a first step towards a more complete model of the
Universe creation – proving that creation Ex Nihilo is feasible. Further adjustments, elaborations, formalisms
and experiments are required to formulate and support the theory.
The “necessary observer” that quantum mechanics require is described in the b...Julio Banks
This essay is intended to share the vies of the author of his Judeo-Christian belief and the physical validation of such believes based upon the theories of Quantum Mechanics.
A fund way to remember how to "fix our manifested creation" by means of observation is as follows: "Keep an eye on the ball", "Do not drop the ball"
Advances in fatigue and fracture mechanics by grzegorz (greg) glinkaJulio Banks
Professor Grzegorz (Greg) Glinka has made substantial contributions to the field of stress concentration evaluation using linear FEA results using the ESED (Equivalent Striain Energy Density). ESED aka Glinka methods allows the determination of strain-stress state at a point of local concentration by equating the strain energy from the linear FEA area in the material strain-stress curve to that of the actual strain-stress of the material using a models such as Ramberg-Osgood. The ESED method is more accurate than the Neuber requiring the equating of SED (Strain Energy Densities) of linear FEA results that Stress is proportional to strain even when the FEA predicts a stress greater than the ultimate strength of the material. One easy method of remember when to use ESED versus Neuber is that ESED, more accurate, should be use on the stress analysis of rocket structures and Neuber delegated to aerospace engines and components.
Digital Twins Computer Networking Paper Presentation.pptxaryanpankaj78
A Digital Twin in computer networking is a virtual representation of a physical network, used to simulate, analyze, and optimize network performance and reliability. It leverages real-time data to enhance network management, predict issues, and improve decision-making processes.
Mechatronics is a multidisciplinary field that refers to the skill sets needed in the contemporary, advanced automated manufacturing industry. At the intersection of mechanics, electronics, and computing, mechatronics specialists create simpler, smarter systems. Mechatronics is an essential foundation for the expected growth in automation and manufacturing.
Mechatronics deals with robotics, control systems, and electro-mechanical systems.
Applications of artificial Intelligence in Mechanical Engineering.pdfAtif Razi
Historically, mechanical engineering has relied heavily on human expertise and empirical methods to solve complex problems. With the introduction of computer-aided design (CAD) and finite element analysis (FEA), the field took its first steps towards digitization. These tools allowed engineers to simulate and analyze mechanical systems with greater accuracy and efficiency. However, the sheer volume of data generated by modern engineering systems and the increasing complexity of these systems have necessitated more advanced analytical tools, paving the way for AI.
AI offers the capability to process vast amounts of data, identify patterns, and make predictions with a level of speed and accuracy unattainable by traditional methods. This has profound implications for mechanical engineering, enabling more efficient design processes, predictive maintenance strategies, and optimized manufacturing operations. AI-driven tools can learn from historical data, adapt to new information, and continuously improve their performance, making them invaluable in tackling the multifaceted challenges of modern mechanical engineering.
Home security is of paramount importance in today's world, where we rely more on technology, home
security is crucial. Using technology to make homes safer and easier to control from anywhere is
important. Home security is important for the occupant’s safety. In this paper, we came up with a low cost,
AI based model home security system. The system has a user-friendly interface, allowing users to start
model training and face detection with simple keyboard commands. Our goal is to introduce an innovative
home security system using facial recognition technology. Unlike traditional systems, this system trains
and saves images of friends and family members. The system scans this folder to recognize familiar faces
and provides real-time monitoring. If an unfamiliar face is detected, it promptly sends an email alert,
ensuring a proactive response to potential security threats.
Software Engineering and Project Management - Introduction, Modeling Concepts...Prakhyath Rai
Introduction, Modeling Concepts and Class Modeling: What is Object orientation? What is OO development? OO Themes; Evidence for usefulness of OO development; OO modeling history. Modeling
as Design technique: Modeling, abstraction, The Three models. Class Modeling: Object and Class Concept, Link and associations concepts, Generalization and Inheritance, A sample class model, Navigation of class models, and UML diagrams
Building the Analysis Models: Requirement Analysis, Analysis Model Approaches, Data modeling Concepts, Object Oriented Analysis, Scenario-Based Modeling, Flow-Oriented Modeling, class Based Modeling, Creating a Behavioral Model.
Height and depth gauge linear metrology.pdfq30122000
Height gauges may also be used to measure the height of an object by using the underside of the scriber as the datum. The datum may be permanently fixed or the height gauge may have provision to adjust the scale, this is done by sliding the scale vertically along the body of the height gauge by turning a fine feed screw at the top of the gauge; then with the scriber set to the same level as the base, the scale can be matched to it. This adjustment allows different scribers or probes to be used, as well as adjusting for any errors in a damaged or resharpened probe.
1. MathCAD - Advection-convection Heat Transfer.xmcd
Thermal Balance on a Fluid Flow Conduit
by Julio C. Banks, PE
Reference
"Heat Transfer" 10th Ed. J. P. Holman
IISBN 978–960–'9607–96352936–963 or MHID 0–9607–96352936–962.
Pp. 21-23.
The intent of this paper is to show the modeling of a heat balance in a conduit with
convection heat transfer and the moving of the transferred energy via advection,
Note: The author has found it to be practical to distinguish Q, and q as "Total heat
transfer flow" and "Heat transfer flux", respectively. This clarification is very important
in the modeling of convection with advection, Some authors fail to name the transfer
of thermal energy via a moving (working) fluid as qa wCp ΔTB=
The energy transfer expressed by Equation (1-8) is used for evaluating the convection
loss for flow over an external surface. Of equal importance is the convection gain or loss
resulting from a fluid flowing inside a channel or tube as shown in Figure 1-8. In this
case, the heated wall at Tw loses heat to the cooler fluid, which consequently rises in
temperature as it flows through the conduit from inlet conditions at Ti to exit conditions
at Te. Using the symbol i to designate enthalpy (to avoid confusion with h, the
convection coefficient), the energy balance on the fluid is
Figure 1-8 Convection and advection in a channel of length L
Qw w ie ii =
Where w is the is the fluid mass flow rate. For many single-phase liquids and gases
operating over reasonable temperature Δi CpΔTB= ranges and e have
Qw w Cp TBe TBi = TBe TBi 1( )
Qh Ah Tw TB = Tw TB 2( )
Equation 2 uses the mean temperature of the wall and that of the bulk fluid.
Julio C. Banks, PE Sell-A-Vision@Outlook.com page 1 of 2
2. MathCAD - Advection-convection Heat Transfer.xmcd
Equating A heat balance is obtained by equation Eq. 1 to Eq. 2 as follows
Qw Qh=
w Cp TBe TBi Ah Tw TB = 1 8a( )
Introduce the concept of "Heat flux", q
Q
A
= , into Eq. 1-8a by dividing it by the heat
transfer surface area, A.
w
A
Cp TBe TBi h Tw TB = 1 8b( )
Let G
w
A
= 1 8c( )
GCp TBe TBi h Tw TB = 1 8d( )
We must be careful to distinguish between the surface area for convection that is
employed in convection Equation (1-8) and the cross-sectional area that is used
to calculate the flow rate from
w ρuAc= 3( )
For a circular conduit, the fluid flow area and the heat transfer surface area are
Ac
π
4
d
2
= 4( )
A πdL= 5( )
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