Investigation of certain techniques for stabilizing detonationwaves in a supersonic flow

Author:

Zhuravskaya T. A.,Levin V. A.

Publisher

Pleiades Publishing Ltd

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Reference13 articles.

1. A.N. Kraiko, “Theoretical and Experimental Validation of the Concept of a Pulsed Engine with a Detonation Wave Moving counter a Supersonic Flow,” in: S.M. Frolov (ed.), Pulsed Detonation Engines [in Russian], Torus Press, Moscow (2006), p. 569.

2. V.A. Levin, V.V. Markov, T.A. Zhuravskaya, and S.F. Osinkin, “Initiation, Propagation, and Stabilization of Detonation Waves in a Supersonic Flow,” in: A.A. Barmin (ed.), Problems of Modern Mechanics. On the 85-th Birthday of Academician G.G. Chernyi [in Russian], Moscow Univ. Press & Omega-L, Moscow (2008), p. 240.

3. Yu.V. Tunik, “Stabilization of Detonation Combustion in a High-Velocity Flow of a Hydrogen-Oxygen Mixture,” Fluid Dynamics 43(6), 954 (2008).

4. Yu.V. Tunik, “Numerical Modeling of Detonation Combustion of Hydrogen-Air Mixtures in a Convergent-Divergent Nozzle,” Fluid Dynamics 45(2), 264 (2010).

5. Yu.V. Tunik, “Stability of Detonation Combustion with Respect to the Variation in the Hydrogen Concentration at the Supersonic Nozzle Inlet,” Fluid Dynamics 46(1), 115 (2011).

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