Experimental investigation of acoustic self-oscillation influence on decay process for underexpanded supersonic jet in submerged space

Author:

Aleksandrov V. Yu.,Arefyev K. Yu.,Ilchenko M. A.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Reference20 articles.

1. V.S. Zuev and V.S. Makaron, Theory of Direct Jet and Ramjet Engines, Mashinostroenie, Moscow, 1971.

2. O.V. Guskov and V.I. Kopchenov, Simulation of flow structure in a channel with supersonic inlet conditions, Aeromechanics and Gasdynamics, 2001, No. 1, P. 28-39.

3. S.I. Baranovsky, V.M. Levin, A.S. Nadvorsky, and A.I. Turishchev, Experimental and theoretical study for co-current supersonic jets with interaction, Int. school-seminar “Turbulent Flows in Interacting Flows”, Minsk, ITMO AS BSSR, 1986, P. 84-98.

4. V.Yu. Aleksandrov, K.Yu. Arefyev, and A.V. Voronetsky, Study of effective regenerative cooling system in supersonic ramjet engines using hydrocarbon fuel, Teplovye Processy v Tekhnike, 2014, Vol. 6, No. 11, P. 489-495.

5. V.I. Tsutsuran, N.V. Petrukhin, and S.A. Gusev, Military and Technical Analysis of State of Art and Perspectives in Field of Rocket Fuel, DM RF, Moscow, 1999.

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