Mathematical model of the supersonic heterogeneous flow incident on a flat obstacle


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Abstract

A mathematical model for a supersonic heterogeneous flow incident on a flat obstacle and a model for calculating the inertial motion of particles of the supersonic heterogeneous flow through a shock wave and a compressed layer are described in this paper. Possible modes and variants of the inertial motion of particles in the compressed layer are analyzed. A dependence is derived to estimate the velocity of particles after their propagation through the shock wave and the compressed layer. The practical application of the obtained results is proposed.

About the authors

P. V. Nikitin

Moscow Aviation Institute (National Research University)

Email: gljul@bk.ru
Russian Federation, Moscow, 125993

S. A. Borisov

Moscow Aviation Institute (National Research University)

Email: gljul@bk.ru
Russian Federation, Moscow, 125993

S. V. Dobrovolskiy

Moscow Aviation Institute (National Research University)

Email: gljul@bk.ru
Russian Federation, Moscow, 125993

Yu. I. Glukhovskaya

Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: gljul@bk.ru
Russian Federation, Moscow, 125993

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