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Books on the topic 'Heat engine combustion chamber'

Author: Grafiati

Published: 30 May 2022

Last updated: 31 July 2025

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1

M, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.

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2

M, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.

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3

M, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.

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4

A, Roncace Elizabeth, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Hot-gas-side heat transfer characteristics of subscale, plug-nozzle rocket calorimeter chamber. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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5

Quentmeyer, Richard J. Hot-gas-side heat transfer characteristics of subscale, plug-nozzle rocket calorimeter chamber. Lewis Research Center, 1993.

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6

United States. National Aeronautics and Space Administration., ed. Heat transfer in rocket engine combustion chambers and regeneratively cooled nozzles: Final report. SECA, Inc., 1993.

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7

United States. National Aeronautics and Space Administration., ed. Heat transfer in rocket engine combustion chambers and regeneratively cooled nozzles: Final report. SECA, Inc., 1993.

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8

Jankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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9

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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10

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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11

D, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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12

S, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. National Aeronautics and Spac14., 1988.

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13

Masters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Lewis Research Center, 1988.

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14

S, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. National Aeronautics and Spac14., 1988.

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15

Don, Hoying, and Universities Space Research Association, eds. Supersonic combustion engine testbed: Heat lightning. Universities Space Research Association, 1990.

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16

S, Jankovsky Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Structurally compliant rocket engine combustion chamber: Experimental and analytical validation. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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17

Berger, F. C. Heat transfer from propellant burning in a constant-volume chamber. Department of Aerospace Science and Engineering, University of Toronto, 1990.

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18

Vecchiarelli, Jack. A proposed combustion chamber for approximating an isothermal heat addition process. National Library of Canada = Bibliothèque nationale du Canada, 1992.

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19

Shannon, Vinyard, Keribar Rifat, United States. Dept. of Energy. Office of Vehicle and Engine Research and Development., and United States. National Aeronautics and Space Administration., eds. The effect of insulated combustion chamber surfaces on direct-injected diesel engine performance, emissions, and combustion. U.S. Dept. of Energy, Office of Vehicle and Engine R & D, 1989.

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20

William, Brown. Orbit transfer rocket engine technology program: Enhanced heat transfer combustor technology : final report. NASA-Lewis Research Center, 1991.

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21

American Society of Mechanical Engineers. Internal Combustion Engine Division. Technical Conference. New engine technology for cogeneration: Presented at the Internal Combustion Engine Division Technical Conference, Kansas City, Missouri, October 4-7, 1987. American Society of Mechanical Engineers, 1987.

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22

L, Yang S., Schock H. J, Society of Automotive Engineers, and Lewis Research Center, eds. A two-dimensional numerical study of the flow inside the combustion chamber of a motored rotary engine. Society of Automotive Engineers, 1986.

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23

A, Willis Edward, and United States. National Aeronautics and Space Administration., eds. Performance of a supercharged direct-injection stratified-charge rotary combustion engine. NASA, 1990.

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24

Bagabir, A. M. Numerical simulation of two-dimensional flow and heat transfer around a hexagonal-shaped combustion chamber. UMIST, 1997.

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25

K, Shaltens Richard, and United States. National Aeronautics and Space Administration., eds. Automotive stirling engine development project. National Aeronautics and Space Administration, 1997.

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26

CRC Deposit Group. Combustion Chamber Deposit Panel., ed. Literature search on the impact of combustion chamber deposits on engine performance (CRC Project No. CM-136-95). Coordinating Research Council, 1995.

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27

Thomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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28

Thomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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29

Thomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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30

Lee, Nguyen Hung, and United States. National Aeronautics and Space Administration., eds. Performance and efficiency evaluation and heat release study of an outboard marine corporation rotary combustion engine. National Aeronautics and Space Administration, 1987.

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31

Rasooli-Nejad, Seyed H. Predictions of heat transfer in a direct-injection diesel engine based on high-speed photographs of combustion. UMIST, 1998.

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32

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. National Aeronautics and Space Administration, 1997.

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33

Marable, R. W. Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle. Pratt and Whitney Aircraft, 1989.

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34

United States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. National Aeronautics and Space Administration, 1997.

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35

Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. Turbine engine hot section technology 1986: Proceedings of a conference. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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36

Heat transfer in rocket engine combustion chambers and regeneratively cooled nozzles. SECA, Inc., 1993.

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37

Heat transfer in rocket engine combustion chambers and regeneratively cooled nozzles. SECA, Inc., 1993.

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38

A Numerical Study of Combined Convective and Radiative Heat Transfer in a Rocket Engine Combustion Chamber. Storming Media, 2002.

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39

Numerical Study of the Effect of the Fuel Film on Heat Transfer in a Rocket Engine Combustion Chamber. Storming Media, 2003.

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40

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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41

Lederer, Gregor. Rocket Engine on a Student Budget. Technische Universität Dresden, 2021. http://dx.doi.org/10.25368/2022.406.

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Abstract:

A technical project alongside the University courses can deepen the understanding and increase the motivation for the subject of choice. As a student, there is often a hurdle to start such a project because of a lack of inspiration. And even after overcoming this, the costs associated with such a project may put students off. With my project I show how a 3rd semester Mechanical Engineering student can design and manufacture a rocket engine with all testing components on a student budget. Cost structure and resource planning are explained in detail. I launched the project in December 2020 and i

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42

National Aeronautics and Space Administration (NASA) Staff. Supersonic Combustion Engine Testbed, Heat Lightning. Independently Published, 2018.

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43

Evans, R. L. Combustion chamber design for a Lean-Burn SI engine. Society of Automotive Engineers., 1992.

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44

SSME Main Combustion Chamber (MCC) 'hot oil' dewaxing. National Aeronautics and Space Administration, 1994.

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45

Modeling Engine Spray and Combustion Processes (Heat and Mass Transfer). Springer, 2003.

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46

A two-dimensional numerical study of the flow inside the combustion chamber of a motored rotary engine. Society of Automotive Engineers, 1986.

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47

Busch, Stephen. The Theory and Application of Optical Diagnostic Techniques in the Combustion Chamber of a Diesel Engine. Logos Verlag Berlin, 2013.

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48

Design Study of Triggered Isomer Heat Exchanger-Combustion Hybrid Jet Engine for High Altitude Flight. Storming Media, 2002.

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49

RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.

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50

Analysis of the Application of a Triggered Isomer Heat Exchanger as a Replacement for the Combustion Chamber in an Off-the-Shelf Turbojet. Storming Media, 2001.

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