Engine system performance of pulse detonation concepts using the NPSS program

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

Volumn , Issue , 2002, Pages

  Petters, Dean P ^a   Felder, James L ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BYPASS RATIO; NOZZLES; PROPULSION; PULSE DETONATION ENGINES; RAMJET ENGINES; SHOCK TUBES;

CONSTANT-VOLUME COMBUSTIONS; DETONATION CHAMBERS; ENGINE PRESSURE RATIO; NUMERICAL PROPULSION SYSTEM; PERFORMANCE IMPACT; SPECIFIC FUEL CONSUMPTION; TEMPERATURE AND PRESSURES; UNSTEADY FLOW CHARACTERISTICS;

COMBUSTION KNOCK;

EID: 85088183297     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-3910     Document Type: Conference Paper

References (2)

1. NPSS User Guide and Reference, Revision L, May 2000, P 1-1.
2. Bussing, T. and Pappas, G., "An Introduction to Pulse Detonation Engines, " AIAA 94-0263, 32nd Aerospace Sciences Meeting and Exhibit, Jan 10-13, 1994, Reno, NV.