Log in

Relevant bibliographies by topics / Combustion chambre / Books

To see the other types of publications on this topic, follow the link: Combustion chambre.

Books on the topic 'Combustion chambre'

Author: Grafiati

Published: 28 June 2021

Last updated: 29 July 2025

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 50 books for your research on the topic 'Combustion chambre.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse books on a wide variety of disciplines and organise your bibliography correctly.

1

Council, Coordinating Research, Coordinating Research Council. Performance Committee., and CRC Deposit Group. Combustion Chamber Deposit Program Panel., eds. Combustion chamber deposit research tool development. Coordinating Research Council, 2002.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

2

J, Przekwas A., and United States. National Aeronautics and Space Administration., eds. Combustion chamber analysis code: Final report. CFD Research Corp., 1993.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

3

Center, Lewis Research, ed. Fluids and combustion facility--combustion integrated rack. National Aeronautics and Space Administration, Lewis Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

4

Grigorʹev, A. V. Teorii︠a︡ kamery sgoranii︠a︡. Nauka, 2010.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

5

Quentmeyer, Richard J. Rocket combustion chamber life-enhancing design concepts. National Aeronautics and Space Administration, Lewis Research Center, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

6

Moon, H. J. Soot generation in a diesel combustion chamber. UMIST, 1996.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

7

Hu, Tin Cheung John. An experimental and computational investigation of an annular reverse-flow combustor. University of Toronto, 1991.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

8

Tamaru, Takashi. Hydrogen fueled subsonic-ram-combustor model tests for an air-turbo-ram engine. National Aerospace Laboratory, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

9

Shyy, W. A numerical study of flow in gas-turbine combustor. AIAA, 1987.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

10

Gafurov, R. A. Diagnostika vnutrikamernykh prot͡s︡essov v ėnergeticheskikh ustanovkakh. "Mashinostroenie", 1991.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

11

Jacobs, P. A. Flow establishment in a generic scramjet combustor. Institute for Computer Applications in Science and Engineering, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

12

Association, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. National Fire Protection Association, 2004.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

13

Association, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. National Fire Protection Association, 2004.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

14

Association, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. National Fire Protection Association, 2004.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

15

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. National Aeronautics and Space Administration, 1995.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

16

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. National Aeronautics and Space Administration, 1995.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

17

J, Priem Richard, and United States. National Aeronautics and Space Administration., eds. Analysis of 5 KHz combustion instabilities in 40K methane/LOX combustion chambers. National Aeronautics and Space Administration, 1988.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

18

Kudinov, Anatoliy, Svetlana Ziganshina, and Kirill Husainov. Calculation of thermal schemes of combined-cycle gas installations of thermal power plants. INFRA-M Academic Publishing LLC., 2023. http://dx.doi.org/10.12737/1865669.

Full text

Abstract:

The fundamentals of the theory of increasing the thermal efficiency of power plants through the use of gas turbine and combined-cycle technologies are presented. The classification is given, the basic and calculated thermal schemes, parameters and characteristics of gas turbine and combined-cycle gas installations of various types are given, the principles of their operation are described. The designs of combustion chambers and features of fuel combustion in the combustion chambers of gas turbine installations are given. Methods and examples of calculation of thermal schemes of gas turbine ins

APA, Harvard, Vancouver, ISO, and other styles

19

Bement, David A. Measured operating characteristics of a rectangular combustor/inlet isolator. American Institute of Aeronautics and Astronautics, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

20

Colannino, Joseph. Modeling of combustion systems: A practical approach. CRC/Taylor & Francis, 2006.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

21

1926-, Rosenberg S. D., and Lewis Research Center, eds. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. GenCorp, Aerojet, 1991.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

22

R, Hicks Yolanda, Hanson Ronald K, and United States. National Aeronautics and Space Administration., eds. AST combustion workshop: Working group report. National Aeronautics and Space Administration, 1996.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

23

Libbis, N. Coal particle behaviour in a counter-current combustor. Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1987.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

24

E, Smith C., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. CFD assessment of orifice aspect ratio and mass flow ratio on jet mixing in rectangular ducts. National Aeronautics and Space Administration, 1994.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

25

C, Mongia H., Mularz Edward J, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology Activity., eds. Assessment, development, and application of combustor aerothermal models J.D. Holdeman, H.C. Mongia, and E.J. Mularz. National Aeronautics and Space Administration ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity, 1988.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

26

United States. National Aeronautics and Space Administration., ed. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Aerojet TechSystems, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

27

Syed, Saadat A. Error reduction program: Final report. Lewis Research Center, 1985.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

28

United States. National Aeronautics and Space Administration., ed. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Aerojet TechSystems, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

29

S, Jankovsky Robert, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Hot fire test results of subscale tubular combustion chambers. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

30

Holdeman, J. D. A numerical study of the effects of curvature and convergence on dilution jet mixing. National Aeronautics and Space Administration, 1987.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

31

L, Lee R. S., Whitelaw James H, Wung T. S, and International Union of Theoretical and Applied Mechanics., eds. Aerothermodynamics in combustors: IUTAM Symposium, Taipei, Taiwan, 1991. Springer-Verlag, 1992.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

32

R, Hicks Yolanda, Hanson Ronald K, and United States. National Aeronautics and Space Administration., eds. AST combustion workshop: Diagnostic working group report. National Aeronautics and Space Administration, 1996.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

33

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.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

34

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.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

35

C, Farmer Richard, and United States. National Aeronautics and Space Administration, eds. SSME main combustion chamber and nozzle flowfield analysis: Final report. National Aeronautics and Space Administration, 1986.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

36

A, Jeroszko Ronald, Kennedy J. B, and Lewis Research Center, eds. Broad specification fuels combustion technology program, phase II: Final report. Lewis Research Center, National Aeronautics and Space Administration, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

37

United States. National Aeronautics and Space Administration., ed. Mixing of multiple jets with a confined subsonic crossflow: Summary of NASA-supported experiments and modeling. National Aeronautics and Space Administration, 1991.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

38

Bose, S. Materials for advanced turbine engines (MATE) project 3 design, fabrication and evaluation of an oxide dispersion strengthened sheet alloy combustor liner. National Aeronautics and Space Administration, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

39

Hu, T. C. J. An experimental and computational investigation of an annular reverse-flow combustor. Institute for Aerospace Studies, University of Toronto, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

40

Eurotherm Seminar (17th 1990 Cascais, Portugal). Heat transfer in radiating and combusting systems: Proceedings of Eurotherm Seminar no. 17, 8-10 October 1990, Cascais, Portugal. Springer-Verlag, 1991.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

41

A, Winsa Edward, and Lewis Research Center, eds. Fluids and combustion facility--fluid integrated rack. National Aeronautics and Space Administration, Lewis Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

42

Center, Langley Research, ed. A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE. National Aeronautics and Space Administration, Langley Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

43

Center, Langley Research, ed. A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE. National Aeronautics and Space Administration, Langley Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

44

L, Yang S., Kundu K. P, and United States. National Aeronautics and Space Administration., eds. Evaluation of water injection effect on NOx formation for a staged gas turbine combustor. American Institute of Aeronautics and Astronautics, 1996.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

45

L, Yang S., Kundu K. P, and United States. National Aeronautics and Space Administration., eds. Evaluation of water injection effect on NOx formation for a staged gas turbine combustor. American Institute of Aeronautics and Astronautics, 1996.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

46

R, Saunders William, Vandsburger Uri, and NASA Glenn Research Center, eds. A design methodology for rapid implementation of active control systems across lean direct injection combustor platforms. National Aeronautics and Space Administration, Glenn Research Center, 2003.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

47

Center, Langley Research, ed. A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE. National Aeronautics and Space Administration, Langley Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

48

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

Find full text

APA, Harvard, Vancouver, ISO, and other styles

49

C, Ehlers Robert, Parrott Edith, and United States. National Aeronautics and Space Administration., eds. NASA Lewis Research Center's Preheated Combustor and Materials Test Facility. National Aeronautics and Space Administration, 1995.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

50

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

Find full text

APA, Harvard, Vancouver, ISO, and other styles

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!