Stationary and dynamic thermal analyses of cryogenic liquid rocket combustion chamber walls

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Riccius, Jörg R ^a   Zametaev, Evgeny B ^a  

^a Fluids and Structures Group (Space Propulsion Branch Technology Section)   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION CHAMBER WALLS; DYNAMIC THERMAL ANALYSIS; LIQUID ROCKET COMBUSTIONS; NONLINEAR DEFORMATIONS; NONLINEAR STRUCTURAL ANALYSIS; ROCKET COMBUSTION CHAMBERS; THERMAL AND MECHANICAL LOADINGS; THERMAL BOUNDARY CONDITIONS;

BOUNDARY CONDITIONS; COOLING; FLUID MECHANICS; PROPULSION; ROCKETS; THERMOANALYSIS;

COMBUSTION CHAMBERS;

EID: 84896693221     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. D. Kuhl, A. Woschnak, and O. J. Haidn. Coupled heat transfer and stress analysis of rocket combution chabers. In AIAA-98-3373, pages 3373-1-3373-10, 1998.
2. D. Kuhl, J. R. Riccius, and O. J. Haidn. Thermomechanical Fluidstructure analysis and mathematical optimization techniques applied to cryogenic liquid rocket engine design. In O. J. Haidn, editor, International Symposium on Liquid Space Propulsion, Heilbronn, 2000.
3. J. Riccius and A. Woschnak. Thermo-Fluid-mechnanical and low cycle fatigue analyses of cryogenic liquid rocket combustion chambers. In NAFEMS-Seminar: Fatigue Analysis, pages 16. 1-16. 8, 2000.
4. J. R. Riccius, M. R. Hilsenbeck, and O. J. Haidn. Optimization of geometric parameters of cryogenic liquid rocket combustion chambers. In 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, pages 3408. 1-11. AIAA, 2001.
5. D. R. Bartz. A simple equation for rapid estimation of rocket nozzle convective heat transfer coefficients. Jet Propulsion, 27: 49-51, 1957.
6. S. C. Fisher, M. Popp, and R. J. Quentmeyer. Thrust chamber cooling and heat transfer. In 2nd Int. Symposium on Liquid Rocket Propulsion, pages 16-1-16-27. ONERA, 1995.
7. A. Woschnak and M. Oschwald. Thermo and fluidmechanical analysis of high aspect ratio cooling channels. In 37th Joint Propulsion Conference and Exhibit. AIAA 2001-3404, Salt Lake City, UT, 2001.
8. J. B. Conway, R. H. Stentz, and J. T. Berling. High-temperature, lowcycle fatigue of advanced copper-base alloys for rocket nozzles; part 1-NARloy-Z. Technical report, NASA-CR-134627, 1974.
9. J. B. Conway, R. H. Stentz, and J. T. Berling. High-temperature, low-cycle fatigue of copper-base alloys for rocket nozzles; part I-data summary for materials tested in prior programs. Technical report, NASACR-134908, 1975.
10. R. T. Cook, E. E. Fryk, and J. F. Newell. SSME main combustion chamber life prediction. Technical report, NASA, 1983.
11. H. F. R. Schöyer. Combustion instability in liquid rocket engines. Technical report, ESA WPP-062, 1993.