533.6:51-71 Investigation of the energy and mass transfer influence on the wake flow of supersonic conical models

Sidnyaev N. I. (Bauman Moscow State Technical University), Gordeeva N. M. (Bauman Moscow State Technical University)

BASE AREA, PRESSURE, BOUNDARY LAYER, HYPERSONIC SPEED, CIRCULATING FLOW, SHOCK WAVE, THE MACH NUMBER.


doi: 10.18698/2309-3684-2015-1-3149


We studied the dynamics of motion and energy transfer in supersonic flow in the base region. It is shown in the article that the current in the base region largely depends on the boundary layer structure in the area between the trailing edge and the sticking point on the centerline, where the boundary layer cut out from the rear edge converges. The study of the effect of gas mass injection into the base region from the body surface and the bottom as well as heat transfer in the bottom region is included. The resulting solution of the problem of the middle wake for axisymmetric body without considering recirculation at a limited distance from the stern has been obtained.


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Sidnyaev N., Gordeeva N. Investigation of the energy and mass transfer influence on the wake flow of supersonic conical models. Маthematical Modeling and Coтputational Methods, 2015, №1 (5), pp. 31-49



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