CFD simulations of a novel multi-tube pulse detonation engine inlet concept
Author:
Affiliation:
1. Prairie View A & M Univ., TX
2. Boeing North America Inc., Rocketdyne Div., Canoga Park, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2240
Reference11 articles.
1. Loth, E., Loth, J., and Loth, F., 1992 "High Efficiency Detonation Internal Combustion Engine,"AL4A Paper 92-3171
2. Eidelman, S., Grossmann,W., and Lottati, I., 1990, " Computational Analysis of Pulse Detonation Engines and Applications ,"ALAA Paper 90-0460
3. Pegg, R.J., Couch , B.D and Hunter, L. G., 1996,"Pulse Detonation Engine Air Induction SystemAnalysis," AlAA Paper 96-2918
4. Bussing, T.R.A., 1995, "A Rotary Valve Multiple Pulse Detonation Engine," AUA Paper 95-2577
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1. Deconstructing Detonation: Analytical Calculation of Unsteady Thrust in a PDE;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26
2. Recent developments in the research on pulse detonation engines;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14
3. Utilization of pressure wave interaction to investigate PDE internal flow paths;37th Joint Propulsion Conference and Exhibit;2001-07-08
4. CFD optimization of a integrated multi-tube PDE/inlet concept using complex variables;17th Applied Aerodynamics Conference;1999-06-28
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