Investigation of aerodynamic characteristics of a hypersonic flow around bodies of revolution with a permeable tip |
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Authors: | N I Sidnyaev |
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Institution: | (1) Bauman Moscow State Technical University, Moscow, 105005 |
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Abstract: | Results of experimental investigations of aerodynamic characteristics of models of high-velocity flying vehicles consisting
of a combination of a blunt cone, a cylinder, and a conical tail fin are presented. The model forebody is cooled by porous
blowing. The choice of such a configuration is determined by the necessity of optimizing the arrangement of high-velocity
flying vehicles on the launcher and their aerodynamic characteristics under conditions of intense surface mass transfer (decrease
in drag and heat transfer and increase in static and dynamic stability).
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Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 48, No. 2, pp. 19–26, March–April, 2007. |
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Keywords: | aerodynamic characteristics mass transfer heat transfer supersonic dynamic stability moment |
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