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 a...
|Published in:||Journal of Applied Mechanics and Technical Physics, Vol. 53, No. 3 (2012), p. 333-339|
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|Item Description:||Original Russian Text © V.M. Fomin, V.I. Zapryagaev, A.V. Lokotko, V.F. Volkov.__________ Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 53, No. 3, pp. 30–37, May–June, 2012.|
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