Thermodynamic cycle and CFD analyses for hydrogen fueled air-breathing pulse detonation engines

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

Volumn , Issue , 2002, Pages

  Povinelli, Louis A ^a   Yungster, Shaye ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR-BREATHING PULSE DETONATION ENGINES; CYCLE PERFORMANCE; FINITE-RATE CHEMISTRY; HYDROGEN-AIR MIXTURE; PERFORMANCE POTENTIALS; STATIC CONDITIONS; THERMODYNAMIC CYCLE; THERMODYNAMIC CYCLE ANALYSIS;

COMPUTATIONAL FLUID DYNAMICS; HYDROGEN; PROPULSION; PULSE DETONATION ENGINES;

THERMODYNAMIC PROPERTIES;

EID: 84896693861     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Povinelli, Louis A., "Impact of Dissociation and Sensible Heat release on Pulse Detonation and Gas Turbine Engine Performance, " NASA/TM-2001, July 2001, also 15th ISABE Symposium Paper 2001-1212, Sept. 2002.
2. Povinelli, L., Lee, J.-H. and Landenberg, M., "Role of Air-Breathing Pulse Detonation Engines in High Speed Propulsion, " NASA/TM-2001-211163, Sept. 2001, also 52nd International Astronautically Congress Paper IAF-01-S. 5. 01, Oct. 2001.
3. Povinelli, Louis A., and Yungster, Shaye, "26th Airbreathing Propulsion Sub committee, " N AS A/TM-20 02-21 157 5, also JANNAF Conference, Airbreathing Pulse Detonation Engine Performance, D es tin, FL, A pr il 8-12, 200 2.
4. Heiser, William. H., and Pratt, David T., "Thermodynamic Cycle Analysis of Pulse Detonation Engines, " Jrl. of Propulsion and Power, Vol. 18, No. 1, January-February 2002.
5. Gordon. S., and McBride. B, "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, Part 1. Analysis, " NASA RP-1311, June 1966.
6. 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.
7. Yungster, S. and Radhakrishnan, K., "Simulation of Unsteady Hypersonic Combustion Around Projectiles in an Expansion Tube, " Shock Waves, Vol. 11, 2001, pp. 167-177.
8. Y un gs ter, S, an d Rad hakr ish nan, K., "Co mp utation al Stud y o f N ear-Lim it P r op ag ation o f D eton ation in H yd ro g en-A ir Mixtu res, " 38th AIAA/AS ME/SA E/ASEE Joint Propulsion Conference, I nd ianap olis, I nd ian a, J u ly 7-1 0, 200 2.
9. Jackomowski, C. J., "An Analytical Study of the Hydrogen-Air Reaction Mechanism with Application to Scramjet Combustion, " NASA TP-2791, Feb. 1988.
10. Schauer, Fred, Stutrud, Jeff, and Bradley, Royce, "Detonation Initiation Studies and Performance Results for Pulse Detonation Engine Applications, " AIAA Paper 2001-1129.
11. Wintenberger, E., Austin, J. M., Cooper, S., and Shepherd, J. E., "An Analytical Model for the Impulse of a Single-Cycle Pulse Detonation Engine, " AIAA Paper 01-34455, July 2001.