Investigation of Unsteady Flow Field in a 2-Stage PDE Resonator

Author:

Leyva Ivett1,Tangirala Venkat1,Dean Anthony1

Affiliation:

1. GE Global Research

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Eidelman, S., and Grossmann, W. "Pulsed Detonation Engine: Experimental and Theoretical review", AIAA paper 92-3168, July

2. 1992. Levin, V.A., Nechaev, J.N., and Tarasov, A.I. "A New Approach to Organizing Operation Cycles in Pulse Detonation Engines", pp.223-238in High-Speed Deflagration and Detonation:Fundamentalsand Control, (Ed. G.D. Roy, S.M. Frolov, D.W. Netzer and A.A. Borisov),Moscow2001.

3. Achasov, O.V., and Penyazkov, O. G. "Some Gasdynamic Method for Control of Detonation Initiation and Propagation", pp.31-44, in High-Speed Deflagration and Detonation:Fundamentalsand Control, (Ed. G.D. Roy, S.M. Frolov, D.W. Netzer and A.A. Borisov),Moscow2001.

4. Gutmark, E., Schadow, K.C., Wilson, K.J., Bicker, C.J. `Near-field pressure radiation and flow characteristics in low supersonic circular andellipticjets',Phys.Fluids31(9),Sept.1988.

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