Pulse detonation engine air induction system analysis

32nd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1996, Pages

  Pegg, Robert J ^a   Couch, B D ^b   Hunter, L G ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; ETHYLENE; EXPLOSIVES; FIGHTER AIRCRAFT; INTAKE SYSTEMS; JET ENGINES; MACH NUMBER; NASA; NAVIER STOKES EQUATIONS; PROPULSION; SUPERSONIC AIRCRAFT; TURBULENCE MODELS;

AIR INDUCTION SYSTEMS; BASELINE CONFIGURATIONS; COMPONENT PERFORMANCE; MIXED COMPRESSIONS; TACTICAL AIRCRAFTS; TIME-DEPENDENT ANALYSIS; TOTAL PRESSURE RECOVERY; TWO-DIMENSIONAL APPROXIMATION;

PULSE DETONATION ENGINES;

EID: 84961924298     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Hunter, L. G.; Couch, B. D.; Domel, N. D.; and Winfree, D. D.: Pulse Detonation Concepts. General Dynamics Fort Worth Division ERR-FW- 4339,1995.
2. Bratkovich, T. E.; and Bussing, T. R. A: A Pulse Detonation Engine Performance Model. AIAA 953155, July 1995.
3. Bussing, T. R. A.; and Pappas, G.: An Introduction to Pulse Detonation Engines. AIAA 94-0263, January 1994.
4. Hunter, L. G.; and Couch, B. D.: Air Injection System Integration Study for Pulse Detonation Engines. Lockheed Martin Tactical Aircraft Systems FZM-8382, October 1995.
5. Pegg, R. J.; Hunt, J. L.; et al.: Design of a Hypersonic Waverider-Derived Airplane. AIAA 93-0401,1993.
6. Hunter, L. G. and Winfree, D. D.: Pulse Detonation Engine U.S. Patent, 5, 473-885; 1995.
7. Bussing, T. R. A.: Rotary Valve Multiple Combustor Pulse Detonation Engine. U.S. Patent, 5, 345-758; 1994.
8. Reed, C. J.: Central Difference FALCON User’s Manual. Lockheed Martin Tactical Aircraft Systems, 1994.
9. Smith, B. R.: Prediction of Hypersonic Shock Wave Turbulent Boundary-Layer Interactions with the K-L Two Equation Turbulence Model. AIAA 95-0232,1995.
10. Miller, D. R. and Hamstra, J. W.: A Computational Assessment of Surge-Induced Inlet OverPressure Distribution for Preliminary Design. ASME 96-67-548.
11. Cambier, J. J. and Adelman, H. G.: Preliminary Numerical Simulations of a Pulse Detonation Wave Engine. AIAA 88-2960,1988.