The thermodynamic basis of pulsed detonation engine thrust production

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

Volumn , Issue , 2002, Pages

  Dyer, R S ^a   Kaemming, T A ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPONENT EFFICIENCIES; CONSERVATION OF ENERGY; FUEL-TO-AIR RATIO; PULSED DETONATION ENGINE; THERMODYNAMIC CYCLE; THERMODYNAMIC MODEL;

DETONATION; PROPULSION; THERMODYNAMIC PROPERTIES;

ENGINES;

EID: 84896693930     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. A. Wortman, P. Othmer and W. Rostafinski, (1992) "Detonation Duct Gas Generator Demonstration Program, " AIAA 92-3174.
2. T. Bussing and G. Pappas, (1996) "Pulse Detonation Engine Theory and Concepts, " Developments in High-Speed-Vehicle Propulsion Systems, AIAA Vol. 165, Progress in Astronautics and Aeronautics, pp. 421-472.
3. W. H. Heiser and D. T. Pratt, (2002) "Thermodynamic Cycle Analysis of a Pulse Detonation Engine, " Journal of Propulsion and Power, Vol. 18, No. 1, pp. 68-76.
4. A. H. Shapiro, The Dynamics and Thermodynamics of Compressible Flow, Vol. 1, John Wiley & Sons, New York, 1953, pp. 193-203.
5. R. A. Strehlow, Combustion Fundamentals, McGraw-Hill, New York, 1984, pp. 304-307.