This presentation is the extension of the first presentation of the same title. It describes the design, mathematically equation, PDF table generation for combustion, simulation, and results of it.
in this presentation , the different engine inefficiencies has been discussed including all sort of friction losses which affects the brake power of the engine. It includes volumetric efficiency, thermal efficiency, IMEP, BMEP, brake power etc.
Technological advancements in IC enginesSyed Yaseen
This presentation is a part of IC engines online course where you will learn about the Technological advancements in IC engines. All the slides are filled with related graphics to help you understand the concept easily.
The gas turbine is an internal combustion engine that uses air as the working fluid. The engine extracts chemical energy from fuel and converts it to mechanical energy using the gaseous energy of the working fluid (air) to drive the engine and propeller, which, in turn, propel the airplane.
in this presentation , the different engine inefficiencies has been discussed including all sort of friction losses which affects the brake power of the engine. It includes volumetric efficiency, thermal efficiency, IMEP, BMEP, brake power etc.
Technological advancements in IC enginesSyed Yaseen
This presentation is a part of IC engines online course where you will learn about the Technological advancements in IC engines. All the slides are filled with related graphics to help you understand the concept easily.
The gas turbine is an internal combustion engine that uses air as the working fluid. The engine extracts chemical energy from fuel and converts it to mechanical energy using the gaseous energy of the working fluid (air) to drive the engine and propeller, which, in turn, propel the airplane.
various methods for improving the engine performance have been discussed. Most significant upon them is to reduce the obstruction in the flow of fresh mixture and burnt products. In addition to this by improving the inlet and exhaust valve timing. Increase in compression ratio and swept volume may also improve the engine parformance
various methods for improving the engine performance have been discussed. Most significant upon them is to reduce the obstruction in the flow of fresh mixture and burnt products. In addition to this by improving the inlet and exhaust valve timing. Increase in compression ratio and swept volume may also improve the engine parformance
CFD ANALYSIS IN AN EJECTOR OF GAS TURBINE ENGINE TEST BEDIAEME Publication
An Ejector system has been used to provide high mass flow to the aero-gas turbine engine in a ground test bed facility. CFD method has been used to determine the performance of the ejector with and without a debris guard. In the first case of flow analyses without debris guard in the ejector, the back pressure was reduced to an extent to know the entrainment ratio. It was found that a pressure of 0.1 bar is required to attain this condition called double choking of the ejector. Further analysis was carried out for a back pressure of 0.9 bar with debris guard. Total pressure loss of 8.56% was found across the debris guard. Also the mass flow through the ejector has reduced by 15% due to debris guard.
Experimental Analysis of Refrigeration system using Microchannel condenser & ...AM Publications
Micro channel condenser now days can be effectively used due to its compact size in automobile sector. For
its performance, refrigeration set up designed to detect experimental performance of microchannel condenser. In this
paper performance analysis of microchannel condenser compared with round tube and coil tube. In analysis of
microchannel condensers it can be found more effective at various loads and operating conditions. For review same size of
microchannel and round tube condenser are considered. From the previous experiments the micro-channel condenser was
made to have nearly an identical face area, depth and fin density as the round-tube condenser which was the baseline. Also
varying the refrigerants, C.O.P & Efficiency of micro channel the various reviews of reviewer micro channel condenser
can be efficient and also refrigerator system requires less power.
Experimental investigate to obtain the effectiveness of regenerator using Air.IJESFT
The regenerator is a kind of heat exchanger that provides a way to get the gas to the low temperature with as much potential work (cooling power) as possible without carrying a lot of heat with it. It doesn’t put heat in or out of the system but it absorbs heat from the gas on one part of the pressure cycle and returns heat to the gas on the other part.
More recent applications of regenerators in cryogenic systems can be found in small cryogenic refrigerators (cryocoolers). Systems such as the Stirling Gifford-McMahon, pulse tube, Solvay, Vuilleumier and magnetic cycle refrigerators all use either a static or rotary regenerator. In fact, the success these coolers have achieved is directly related to the characteristics of compact size and efficiency of the regenerator.
Regenerator effectiveness of 99% results in 21% loss of refrigeration effect, similarly regenerator effectiveness of 98% results in 42% loss of refrigeration effect, with refrigeration effectiveness of 95.238% the loss of refrigeration is 100%. i.e. no net cooling is produced.
In cryogenic applications the regenerator is typically made up of 100 to 500 meshes SS 304, Phosphorous bronze screens or small lead spheres (150 to 300 micro meters) are used, that are tightly packed together and held in place on either end in the same manner.
To develop experimental setup at our laboratory level by using air as working fluid and find out the effectiveness of various regenerative materials is basic goal of this work.
The International Journal of Engineering & Science is aimed at providing a platform for researchers, engineers, scientists, or educators to publish their original research results, to exchange new ideas, to disseminate information in innovative designs, engineering experiences and technological skills. It is also the Journal's objective to promote engineering and technology education. All papers submitted to the Journal will be blind peer-reviewed. Only original articles will be published.
The papers for publication in The International Journal of Engineering& Science are selected through rigorous peer reviews to ensure originality, timeliness, relevance, and readability.
LES Analysis on Confined Swirling Flow in a Gas Turbine Swirl BurnerROSHAN SAH
This presentation describes a Large Eddy Simulation (LES) investigation into flow fields in a model gas turbine combustor equipped with a swirl burner. A probability density function was used to describe the interaction physics of chemical reaction and turbulent flow as liquid fuel was directly injected into the combustion chamber and rapidly mixed with the swirling air. Simulation results showed that heat release during combustion accelerated the axial velocity motion and made the recirculation zone more compact
Preliminary Design of 100 Seater AircraftROSHAN SAH
This presentation explains the different design phases of aircraft and some detailed descriptions of each phase. Then, it explains the preliminary design procedure of the aircraft which consists of weight estimation, wing design, fuselage design, drag polar, maximum speed, thrust requirement and selection of engine, landing gear selection, tail surface design, and different performance calculations.
It explains about flames, types of flames, flame instabilities, stability techniques, and some CFD result of stabilized flame after using different techniques.
This presentation consists of a definition, different instabilities occur due to supersonic flame, Ignition and flame stabilization techniques, Fuel-air mixing enhancement, and problem.
Study on Effect of Semi Circular Dimple on Aerodynamic Characteristics of NAC...ROSHAN SAH
This is the research paper that was published in the AIP Conference Proceedings this year. This paper contains the new modification design in NACA 2412 airfoil and different aerodynamics characteristics were determined and compared with the basic airfoil and multiple conclusion were made for the results.
This was actually my B.Tech. min project work back on 2016 Nov end.
Numerical Investigation of Turbulent Flow Around a Stepped Airfoil at High Re...ROSHAN SAH
It's the extension of the first presentation of it. It contains the results of the stepped airfoils in comparison with the basic airfoil and experimental results.
Numerical Investigation of Turbulent Flow Around a Stepped Airfoil at High Re...ROSHAN SAH
This presentation describes a mathematical investigation of turbulent flow around a stepped airfoil. It includes the design of stepped airfoil, airfoil theory, governing equation of turbulence modeling and boundary condition. whereas, results and discussion are shown in second presentation on same topic.
Courier management system project report.pdfKamal Acharya
It is now-a-days very important for the people to send or receive articles like imported furniture, electronic items, gifts, business goods and the like. People depend vastly on different transport systems which mostly use the manual way of receiving and delivering the articles. There is no way to track the articles till they are received and there is no way to let the customer know what happened in transit, once he booked some articles. In such a situation, we need a system which completely computerizes the cargo activities including time to time tracking of the articles sent. This need is fulfilled by Courier Management System software which is online software for the cargo management people that enables them to receive the goods from a source and send them to a required destination and track their status from time to time.
NO1 Uk best vashikaran specialist in delhi vashikaran baba near me online vas...Amil Baba Dawood bangali
Contact with Dawood Bhai Just call on +92322-6382012 and we'll help you. We'll solve all your problems within 12 to 24 hours and with 101% guarantee and with astrology systematic. If you want to take any personal or professional advice then also you can call us on +92322-6382012 , ONLINE LOVE PROBLEM & Other all types of Daily Life Problem's.Then CALL or WHATSAPP us on +92322-6382012 and Get all these problems solutions here by Amil Baba DAWOOD BANGALI
#vashikaranspecialist #astrologer #palmistry #amliyaat #taweez #manpasandshadi #horoscope #spiritual #lovelife #lovespell #marriagespell#aamilbabainpakistan #amilbabainkarachi #powerfullblackmagicspell #kalajadumantarspecialist #realamilbaba #AmilbabainPakistan #astrologerincanada #astrologerindubai #lovespellsmaster #kalajaduspecialist #lovespellsthatwork #aamilbabainlahore#blackmagicformarriage #aamilbaba #kalajadu #kalailam #taweez #wazifaexpert #jadumantar #vashikaranspecialist #astrologer #palmistry #amliyaat #taweez #manpasandshadi #horoscope #spiritual #lovelife #lovespell #marriagespell#aamilbabainpakistan #amilbabainkarachi #powerfullblackmagicspell #kalajadumantarspecialist #realamilbaba #AmilbabainPakistan #astrologerincanada #astrologerindubai #lovespellsmaster #kalajaduspecialist #lovespellsthatwork #aamilbabainlahore #blackmagicforlove #blackmagicformarriage #aamilbaba #kalajadu #kalailam #taweez #wazifaexpert #jadumantar #vashikaranspecialist #astrologer #palmistry #amliyaat #taweez #manpasandshadi #horoscope #spiritual #lovelife #lovespell #marriagespell#aamilbabainpakistan #amilbabainkarachi #powerfullblackmagicspell #kalajadumantarspecialist #realamilbaba #AmilbabainPakistan #astrologerincanada #astrologerindubai #lovespellsmaster #kalajaduspecialist #lovespellsthatwork #aamilbabainlahore #Amilbabainuk #amilbabainspain #amilbabaindubai #Amilbabainnorway #amilbabainkrachi #amilbabainlahore #amilbabaingujranwalan #amilbabainislamabad
Student information management system project report ii.pdfKamal Acharya
Our project explains about the student management. This project mainly explains the various actions related to student details. This project shows some ease in adding, editing and deleting the student details. It also provides a less time consuming process for viewing, adding, editing and deleting the marks of the students.
About
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Technical Specifications
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Democratizing Fuzzing at Scale by Abhishek Aryaabh.arya
Presented at NUS: Fuzzing and Software Security Summer School 2024
This keynote talks about the democratization of fuzzing at scale, highlighting the collaboration between open source communities, academia, and industry to advance the field of fuzzing. It delves into the history of fuzzing, the development of scalable fuzzing platforms, and the empowerment of community-driven research. The talk will further discuss recent advancements leveraging AI/ML and offer insights into the future evolution of the fuzzing landscape.
TECHNICAL TRAINING MANUAL GENERAL FAMILIARIZATION COURSEDuvanRamosGarzon1
AIRCRAFT GENERAL
The Single Aisle is the most advanced family aircraft in service today, with fly-by-wire flight controls.
The A318, A319, A320 and A321 are twin-engine subsonic medium range aircraft.
The family offers a choice of engines
Quality defects in TMT Bars, Possible causes and Potential Solutions.PrashantGoswami42
Maintaining high-quality standards in the production of TMT bars is crucial for ensuring structural integrity in construction. Addressing common defects through careful monitoring, standardized processes, and advanced technology can significantly improve the quality of TMT bars. Continuous training and adherence to quality control measures will also play a pivotal role in minimizing these defects.
COLLEGE BUS MANAGEMENT SYSTEM PROJECT REPORT.pdfKamal Acharya
The College Bus Management system is completely developed by Visual Basic .NET Version. The application is connect with most secured database language MS SQL Server. The application is develop by using best combination of front-end and back-end languages. The application is totally design like flat user interface. This flat user interface is more attractive user interface in 2017. The application is gives more important to the system functionality. The application is to manage the student’s details, driver’s details, bus details, bus route details, bus fees details and more. The application has only one unit for admin. The admin can manage the entire application. The admin can login into the application by using username and password of the admin. The application is develop for big and small colleges. It is more user friendly for non-computer person. Even they can easily learn how to manage the application within hours. The application is more secure by the admin. The system will give an effective output for the VB.Net and SQL Server given as input to the system. The compiled java program given as input to the system, after scanning the program will generate different reports. The application generates the report for users. The admin can view and download the report of the data. The application deliver the excel format reports. Because, excel formatted reports is very easy to understand the income and expense of the college bus. This application is mainly develop for windows operating system users. In 2017, 73% of people enterprises are using windows operating system. So the application will easily install for all the windows operating system users. The application-developed size is very low. The application consumes very low space in disk. Therefore, the user can allocate very minimum local disk space for this application.
Event Management System Vb Net Project Report.pdfKamal Acharya
In present era, the scopes of information technology growing with a very fast .We do not see any are untouched from this industry. The scope of information technology has become wider includes: Business and industry. Household Business, Communication, Education, Entertainment, Science, Medicine, Engineering, Distance Learning, Weather Forecasting. Carrier Searching and so on.
My project named “Event Management System” is software that store and maintained all events coordinated in college. It also helpful to print related reports. My project will help to record the events coordinated by faculties with their Name, Event subject, date & details in an efficient & effective ways.
In my system we have to make a system by which a user can record all events coordinated by a particular faculty. In our proposed system some more featured are added which differs it from the existing system such as security.
Overview of the fundamental roles in Hydropower generation and the components involved in wider Electrical Engineering.
This paper presents the design and construction of hydroelectric dams from the hydrologist’s survey of the valley before construction, all aspects and involved disciplines, fluid dynamics, structural engineering, generation and mains frequency regulation to the very transmission of power through the network in the United Kingdom.
Author: Robbie Edward Sayers
Collaborators and co editors: Charlie Sims and Connor Healey.
(C) 2024 Robbie E. Sayers
Final project report on grocery store management system..pdfKamal Acharya
In today’s fast-changing business environment, it’s extremely important to be able to respond to client needs in the most effective and timely manner. If your customers wish to see your business online and have instant access to your products or services.
Online Grocery Store is an e-commerce website, which retails various grocery products. This project allows viewing various products available enables registered users to purchase desired products instantly using Paytm, UPI payment processor (Instant Pay) and also can place order by using Cash on Delivery (Pay Later) option. This project provides an easy access to Administrators and Managers to view orders placed using Pay Later and Instant Pay options.
In order to develop an e-commerce website, a number of Technologies must be studied and understood. These include multi-tiered architecture, server and client-side scripting techniques, implementation technologies, programming language (such as PHP, HTML, CSS, JavaScript) and MySQL relational databases. This is a project with the objective to develop a basic website where a consumer is provided with a shopping cart website and also to know about the technologies used to develop such a website.
This document will discuss each of the underlying technologies to create and implement an e- commerce website.
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Dr.Costas Sachpazis
Terzaghi's soil bearing capacity theory, developed by Karl Terzaghi, is a fundamental principle in geotechnical engineering used to determine the bearing capacity of shallow foundations. This theory provides a method to calculate the ultimate bearing capacity of soil, which is the maximum load per unit area that the soil can support without undergoing shear failure. The Calculation HTML Code included.
Saudi Arabia stands as a titan in the global energy landscape, renowned for its abundant oil and gas resources. It's the largest exporter of petroleum and holds some of the world's most significant reserves. Let's delve into the top 10 oil and gas projects shaping Saudi Arabia's energy future in 2024.
AKS UNIVERSITY Satna Final Year Project By OM Hardaha.pdf
Design of pulse jet engine for UAV - 2
1. Seminar-2
ROSHAN SAH
USN :- 17AE60R01
M.Tech (1st Year)
Dept. of AerospaceEngineering,
Indian Institute of Technology
Karagpur (IITKGP)30/08/2017 IIT KGP 1
2. Design of the Pulse Jet Engine:-
Design should be done in such away that above formula should be valid.
Valid of above formulas has been verified against a wide number of different and
proven pulsejet designs including the Argus VI and Dynajet.
By taking above reference, following assumption can be taken:-
1. A = 2.2 F
2. Valve area =0.23* Mean cross- sectionalarea
3. L/D =8
4. Numbers of valves=10
5. Numbers of Gaps =10
6. Efficiencyof Valve = 70%
Parameter Magnitude Units
Mean Area 32.258 Cm2
Mean Diameter 6.41 Cm
Mean Volume 1654.292 Cm3
Length of Pulsejet engine 51.283 Cm
Valve Area 7.419 Cm2
Effective Valve area 10.6 Cm2
Diameter of Each Valve 1.162 Cm
Size of gaps 0.635 Cm
Circumference of valve center circle 17.97 Cm
Diameter of Circle 5.723 Cm
Area of inner circle Covering valves 14.65 Cm2
Inlet area 47.809 Cm2
Diameter of Inlet 7.804 Cm
Length of Combustion Section 16.69 Cm30/08/2017 IIT KGP 2
4. Meshing:-
Meshing of PJE
• Meshing process carriedout through the body of the designed pulse jet
engine. ICEM CFD is used to do the meshing of the design Pulse jet
engine
• Type of Meshing:-
1.Structured Meshing
2.Unstructured Meshing
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5. Analysis of PJE:-
• Analysis was done by using ANSYS Fluent.
• Fluent helps us to provide the inlet and the outlet boundary condition.
• The fluent provides stage to performcombustion analysis using PDF Transport
table methods.
• Boundary conditions:-
1.Solver :- pressure based
2.Viscous model:- Standard K- ω model
3. Fluid condition:- ideal gas
4. Density :1.225 kg/m^3
5. Specific heat at constant pressure(Cp); 1005 J/kg k
6.Inlet velocity:- 10- 50 m/s
7.Ambient Temperature:- 300 K
8.Atmospheric pressure:- 1.01* E5 N/m^2
9.Wall condition:- Stationary wall
10.Shear condition:- No slip
11. Species Model :- Non-premixed Combustion
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6. Following equations are used in simulation;
• Continuity equation: ∇.u=0 …………… (1)
• Momentum equation : ρ
Du
Dt
= −
𝜕p
𝜕x
+ ρgx +µ (∂2u/∂x2 + ∂2u/∂y2 + ∂ 2u/∂z2 ) in x
drxn….(2)
• Transportationequation used
k-ω model:- Rate of dissipation
Turbulent Kinetic energy (K)
Rate of increase of K Convective transport Diffusive Transport Rate of generation source term
Dissipation per unit Kinetic energy(ω) Rate of dissipation cross diffusion
Rate of increase of K Convective transport Diffusive Transport Rate of generation source term
30/08/2017 IIT KGP 6
7. Species Model:-
Non-premixed Combustion model:- solves the total enthalpy form of the energy
equation:
Keff = effective conductivity
Jj = diffusionflux of species j
Sh =heat of chemical reaction
Energy transfer
due to conduction
E = h -
𝑃
𝜌
+
𝑉^2
2
species diffusion&
viscous dissipation
30/08/2017 IIT KGP 7
8. • Combustion Equation:-
CH4 +2*(O2 +3.76 N2) CO2 +2* H2O +2*3.76 N2
Theoretical air fuel ratio =
molecular mass of air
𝑚𝑜𝑙𝑒𝑐𝑢𝑙𝑎𝑟 𝑚𝑎𝑠𝑠 𝑜𝑓 𝑓𝑢𝑒𝑙
=
2∗(32+3.76∗28)
12+4∗1
=
274.56
16
= 17.16
30/08/2017 IIT KGP 8
9. Mean Temperature V/s Mean
mixture Fraction
PDF table generation
30/08/2017 IIT KGP 9
10. Result:-
Case-I
Inlet condition :- After combustion
Velocity :- 10m/s Vmax = 19.1 m/s
Exhaust pipe radius :- 32 mm Tmax =1570 K
30/08/2017 IIT KGP 10
11. Case-II
Inlet condition :- After combustion
Velocity :- 10m/s Vmax = 27.1 m/s
Exhaust pipe radius :- 28mm Tmax =1610 K
30/08/2017 IIT KGP 11
12. Case-III
Inlet condition :- After combustion
Velocity :- 20m/s Vmax = 54.27 m/s
Exhaust pipe radius :- 28 mm Tmax =1670 K
30/08/2017 IIT KGP 12
13. Case-IV
Inlet condition :- After combustion
Velocity :- 50m/s Vmax = 136.3 m/s
Exhaust pipe radius :- 28 mm Tmax =1558K
30/08/2017 IIT KGP 13
14. CONCLUSION:-
• It is able to maintain a stable pressure , with the minimum pressure below
atmospheric pressure.
• Design of small size Pulsejet Engines is easy as large numbers of
complex equations are eliminated.
• The thrust can be increasedwith decrease in the diameter of exhaust
pipe for same operating condition.
• For Modeling the running pulsejet in a wind tunnel on a sting is very
feasible and when compared with the experimental wind tunnel data.
• CFD tests show feasibility of building a Pulsejet Engine.
• They are inefficient when operated at low flight velocities.
30/08/2017 IIT KGP 14
15. REFERENCES
[1] Artt, D, Blair, G, RichardsonJ 1982, ‘A Computer Model of a Pulsejet Engine’,
SAE Technical Paper Series, Volume 82 No. 953.
[2] Artt, D, Blair, G, RichardsonJ 1984, ‘Observations on the Design and
Operation of Pulsejet Engines as Derivedfrom an Experimental and Theoretical
Investigation’, SAE Technical Paper Series, Volume 84 No. 422.
[3] Benson, R, Garg, R, Woollatt, D 1964 ‘A Numerical Solution of Unsteady Flow
Problems’, Journal of Mechanical Sciences, Pergamum Press Ltd., Vol. 6.
[4] Fan, Y, Li, J, Wang, J, Zhang, J, Zhang, Y, Experimental investigation on
kerosene/air pneumatic valve pulse detonation engine, Journal of Aerospace
Power. International Journal of Engineering Research& Technology (IJERT)
IJERTIJERT ISSN: 2278-0181 IJERTV3IS090544 Kentfield, J ‘The Potential of
Valveless Pulsejets for Small UAV Propulsion Applications’ AIAA
Journal 1998, No. 3879 .
[6] Ogorelec, B 2005, Valveless Pulsejet Engines 1.5 – a historical review of
valveless pulsejet designs, Terna Information Services, Zagreb Croatia.
[7] Reynst, F H 1961, Pulsating Combustion, Pergamon Press, London ,UK.
[8] Tharatt, C ‘The Propulsive Duct’ Aircraft Engineering, November 1965, pp 327-
337, December 1965, p 359-371 .
[9] Sunnhordvik, A 2007, Valveless Pulse Jet, Accessed 10May 2007.
[10] Simpson, B 2007, The Valveless Pulse Jet, Accessed15April 2007 .
30/08/2017 IIT KGP 15
16. [11] Geng, Tao, Numerical simulation of pulsejet engines., 2007
[12] Zh eng, Fei, Computational investigations of high speed pulsejets., 200 9
[13] Tao Geng ,Comparison between Numerically Simulated and Experimentally
MeasuredFlow field Quantities behind a Pulsejet , Daniel E Paxson, 200 8
[14] http://aardvark.co.nz/pjet/valveless.html
[15] www.pulsejetbook.com
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