Multiple cycle simulation of a pulse detonation engine ejector

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

Volumn , Issue , 2002, Pages

  Yungster, S ^a   Perkins, H D ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUGMENTATION RATIO; AXIAL LOCATIONS; DETONATION TUBES; EJECTOR SYSTEM; HYDROGEN-OXYGEN MIXTURES; MASS FLOW RATE; MULTIPLE CYCLES; STRONG SHOCK WAVES;

PROPULSION; TUBES (COMPONENTS);

EJECTORS (PUMPS);

EID: 84896693228     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Porter, J. L. and Squyers, R. A., "A Summary/Overview of Ejector Augmentor Theory and Performance, " ATC Report No. R-91100/9CR-47A, Sept. 1979.
2. Presz, W., Reynolds, G. and Hunter, C., "Thrust Augmentation with Mixer/Ejector Systems, " AIAA paper 2002-0230, January 2002.
3. Heiser, W. H. and Pratt, D. T., Hypersonic Airbreathing Propulsion, pp. 446-472, American Institute of Aeronautics and Astronautics, Washington, D. C, 1994.
4. Trefny, C. J., "An Air-Breathing Launch Vehicle Concept for Single-Stage-to-Orbit, " AIAA Paper 99-2730, 1999.
5. Yungster, S. and Trefny, C. J., "Analysis of a New Rocket-Based Combined-Cycle Engine Concept at Low Speed, " AIAA paper 99-2393, June 1999.
6. Heiser, W. H. and Pratt, D. T., "Thermodynamic Cycle Analysis of Pulse Detonation Engines, " Jrn. of Propulsion and Power, Vol. 18, No. 1, January-February 2002.
7. Kailasanath, K., "Recent Developments in the Research on Pulse Detonation Engines, " AIAA paper 2002-0470, January 2002.
8. Yungster, S. and Radhakrishnan, K., "A Fully Implicit Time Accurate Method for Hypersonic Combustion: Application to Shock-Induced Combustion Instability, " Shock Waves, Vol. 5, 1996, pp. 293-303.
9. Jachimowski, C. J., "An Analytical Study of the Hydrogen-Air Reaction Mechanism with Application to Scramjet Combustion, " NASA TP-2791, Feb. 1988.
10. Yungster, S. and Radhakrishnan, K., "Computational Study of Near-Limit Propagation of Detonation in Hydrogen-Air Mixtures, " AIAA paper 2002-3712, July 1.
11. McBride, B. J. and Gordon, S., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications. " II. Users Manual and Program.
12. Daniau, E., Zitoun, R., Couquet, C. and Desbordes, D., "Effects of Nozzles of Different Length and Shape on the Propulsion Performance of Pulsed Detonation Engines, " in High-Speed Deflagration and Detonation, Eds. G. D. Roy, S. M. Frolov, D. Netzer and A. Borisov. Moscow, 2001: ELEX-KM Publ. pp 251-262.