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2. Bussing,T.RA, Hinkey, J.B., and &ye, L. "PulseDetonation EnginePreliminary Design Considerations," AIAA-94-3220, 30th AIAAlASMElSAElASEE Joint PropulsionConference,June 1994 Chue, R,Lee,J.H., Scarinci,T.,Papyrin, A., Knystautas,R, "Transition From Fast Deflagration to Detonation Under the InfluenceofWall Obstacles," in Dyzamic Aspects of Detonation, Progress in AstronauticsandAeromutics,Vol. 153,Ed. by Kuhl,A.L., Keyer,J-C, Borisov, A.A., pp. 270-282, 1993. Chue, R., 1994, personal communications. Glassman, Irvin, Conbustion, Academic Press, Inc,SanDiego, 1987,p. 226. Gordon, S., McBride, B.J. "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications. Part 1: Analysis," NASA RP-1311,1994.
3. Detonation pulse engine
4. This work was funded by the U.S. Air Force under contractF33615-93-C-2348. Theauthorswouldliketo thankLt.James ClegernandCol.John Corneyofthe U.S. Air Force, and Mr. Robert PeggofNASA Langley for theirSUPPOK. In additionthe authors would like to thank Dr. Randy Chue, Dr. Harold Beeson, and the staffat NASAWSTFfortheiresistance. Knystautus,R,Guirao,C., Lee,J.H., and Sulmistras,A. "MeasurementsofCellSize in Hydrocarbon-Air Mixtures and Predictions of Critical Tube Diameter, Critical Initiation Energy, and Detonability Limits," Dynamics of Shock Waves, Explosions, and Detonations, Progress in Aeronautics and Astronautics, Volume94,AIM,1983. Shchelkin, KL., SovietPhysicsJournal of Expdrimental and TechnicalPhysics, Vol. 10,p. 823.