Direct-connect ejector ramjet combustor experiment

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Kamhawi, Hani ^a   Krivanek, Thomas M ^a   Thomas, Scott R ^a   Walker, James F ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR EJECTORS; COMBUSTION; COMBUSTORS; EJECTORS (PUMPS); HYDROGEN; HYDROGEN FUELS; MIXERS (MACHINERY); MIXING; PRESSURE DISTRIBUTION; PROPULSION; RAMJET ENGINES; RESEARCH LABORATORIES; ROCKETS; SEA LEVEL;

ENGINE COMPONENTS; GLENN RESEARCH CENTER; HIGH BACK PRESSURE; OPERATIONAL PROCEDURES; PROPULSION SYSTEM; RAMJET COMBUSTORS; ROCKET BASED COMBINED CYCLES; SIMULTANEOUS MIXING AND COMBUSTION;

DIRECT INJECTION;

EID: 85086619385     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-16     Document Type: Conference Paper

References (17)

1. Trefny, C., An Air-Breathing Launch Vehicle Concept for Single-Stage-to-Orbit. AIAA-99-2730, June 1999.
2. Billig, F. S., The Integration of the Rocket with the Ram-Scramjet as a Viable Transatomospheric Accelerator. AIAA 93-7017, 11th International Symposium on Air-Breathing Engines, Sept. 1993.
3. Yungster, S., and Trefny, C. J., Analysis of a New Rocket-Based Combined Cycle Engine Concept at Low Speed. AIAA 99-2393, June 1999.
4. Walker, J. F., Kamhawi, H., Krivanek, T. M., Thomas, S. R., and Smith, T. D., Status of RBCC Direct-Connect Combustor Experiments. JANNAF 2002 APS-III-113, April 8-12, 2002.
5. Colantonio, R. O., Pachlhofer, P. M., Parrott, E. L., and Piendl, B. R., Advanced Combustor Rig at NASA Lewis Research Center's Engine Components Research Laboratory. NASA TM 4546, March 1994.
6. Repas, G. A., Hydrogen-Oxygen Torch Ignitor. NASA TM 106493, March 1994.
7. Grob, R. L., Modern Practice of Gas Chromatography. New York, 1985.
8. Orth, R. C. and Land, H. B., A Production Type GC Analysis System For Light Gases. Journal of Chromatographic Science, Vol. 9, pp 359-363.
9. Orth, R. C., Billig, F. S. and Grenleki, S. E., Measurement Techniques For Supersonic Combustion Testing, Proceedings of the Instrumentation for Airbreathing Propulsion. September 1972.
10. Burkardt, L.A., and Franciscus, L.C., RAMSCRAM-A Flexible Ramjet/Scramjet Engine Simulation Program, NASA TM 102451, June 1990.
11. Steffen, C. J., Bond, R. B., and Edwards, J. R., Three Dimensional CFD Analysis of the GTX combustor. JANNAF 2002 APS-III-114, April 8-12, 2002.
12. Bond, R.B., and Edwards, J., CFD Analysis of the GTX RBCC Combustor in Mode 1 Operation. AIAA-2003-0017, January 6-9, 2003.
13. Tyll, J. S., Chue, R., and Bakos, R. J., Ejector Analysis and Design Code Formulation. GASL Technical Report No. 381.
14. Chue, R., Sabean, J., Tyll, J. S., and Bakos, R. J., Ejector Design Tool Development For Wind Tunnel Model Design. GASL Technical Report No. 383.
15. Anderson, G.Y.,: An Examination of Injector/Combustor Design Effects on Scramjet Performance. NASA paper presented at the 2nd International Symposium on Air Breathing Engines (Sheffield England), March 25-29, 1974.
16. Notham, G.B., and Anderson, G.Y., Supersonic Combustion Ramjet Research at Langley. AIAA 86-0159, Reno, Nevada, 1986.
17. Gordon, S., and McBride, B.J., Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications. NASA-RP-1311, 1994.