CFD spray combustion model for liquid rocket engine injector analyses

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Cheng, Gary ^a   Farmer, Richard ^b  

^a UNIVERSITY OF ALABAMA AT BIRMINGHAM   (United States)

^b SECA Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 79955550401     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. Cheng, G.C., Anderson, P.G., and Farmer, R.C., "Development of CFD Model for Simulating Gas/Liquid Injectors in Rocket Engine Design, " AIAA Paper 97-3228, 1997.
2. Farmer, R.C., Cheng, G.C., Trinh, H., and Tucker, K., "A design Tool for Liquid Rocket Engine Injectors, " AIAA 2000-3499, 2000.
3. Chen, Y.S., "Compressible and Incompressible Flow Computations with a Pressure Based Method, " AIAA Paper 89-0286, 1989.
4. Cheng, G.C., Farmer, R.C., and Chen, Y.S., "Numerical Study of Turbulent Flows with Compressibility Effects and Chemical Reactions, " AIAA Paper 94-2026, 1994.
5. Cheng, G.C., Chen, Y.S., and Wang, T.S., "Flow Distribution Within the SSME Main Injector Assembly Using Porosity Formulation, " AIAA Paper 95-0350, 1995.
6. Nickerson, G.R., et al, "Two-Dimensional Kinetics (TDK) Nozzle Performance Computer Program, " Vols. I-III, Rpt. No. SN91, Software and Engineering Associates, Inc., mar. 1989.
7. Hirschfelder, J.O., et al, "Generalized Equations of State for Gases and Liquids, " IEC, 50, pp.375-385, 1958.
8. Hirschfelder, J.O., et al, "Generalized Excess Functions for Gases and Liquids, " EC, 50, pp.386-390, 1958.
9. Reid, R.C., et al, The Properties of Gases & Liquids, 4th ed., McGraw-Hill, 1987.
10. Gordon, S., and BJ. McBride, "Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman-Jouget Detonations, " NASA-SP-273,1971.
11. Saad, Y, and Schultz, M.H., SIAM Journal of Sci. Stat. Comput., Vol. 7, pp. 856-869, 1986.
12. Telaar, J., Schneider, G., Hussong, J., and Mayer, W., "Cryogenic Jet Injection: Description of Test Case RCM 1, " Proceeding 2nd International Workshop on Rocket Combustion Modeling, Lampoldshausen, Germany, March 25-27, 2001.
13. Vingert, L., and Habiballah, M., "Test Case RCM 2: Cryogenic Spray Combustion at 10 bar at Mascotte, " Proceeding 2nd International Workshop on Rocket Combustion Modeling, Lampoldshausen, Germany, March 25-27, 2001.
14. Thomas, J.L., et al, "Test Case RCM 3: Supercritical Spray Combustion at 60 bar at Mascotte, " Proceeding 2nd International Workshop on Rocket Combustion Modeling, Lampoldshausen, Germany, March 25-27, 2001.
15. Farmer, R.C., Cheng, G.C., and Chen, Y.S., "CFD simulation of Liquid Rocket Engine Injectors: Test case RCM 1, " Proceeding 2nd International Workshop on Rocket Combustion Modeling, Lampoldshausen, Germany, March 25-27, 2001.
16. Farmer, R.C., Cheng, G.C., and Chen, Y.S., "CFD simulation of Liquid Rocket Engine Injectors: Test case RCM 2, " Proceeding 2nd International Workshop on Rocket Combustion Modeling, Lampoldshausen, Germany, March 25-27, 2001.
17. Farmer, R.C., Cheng, G.C., and Chen, Y.S., "CFD simulation of Liquid Rocket Engine Injectors: Test case RCM 3, " Proceeding 2nd International Workshop on Rocket Combustion Modeling, Lampoldshausen, Germany, March 25-27, 2001.
18. Chehroudi, B., et al, "Initial Growth Rate and Visual Characteristics of a Round Jet into a Sub-to Supercritical Environment of Relevance to Rocket, Gas Turbine, and Diesel Engines, " AIAA 99-0206, 1999.