Effect of distributed gas injection on aerodynamic characteristics of a body of revolution in a supersonic flow

Results of experimental and numerical investigations of the effect of gas injection through a permeable porous surface on the drag coefficient of a cone-cylinder body of revolution in a supersonic flow with the Mach number range M h = 3–6 are presented. It is demonstrated that gas injection through...

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Veröffentlicht in:Journal of applied mechanics and technical physics 2012-05, Vol.53 (3), p.333-339
Hauptverfasser: Fomin, V. M., Zapryagaev, V. I., Lokotko, A. V., Volkov, V. F.
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Sprache:eng
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