Mathematical model of the supersonic heterogeneous flow incident on a flat obstacle
- Authors: Nikitin P.V.1, Borisov S.A.1, Dobrovolskiy S.V.1, Glukhovskaya Y.I.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 10, No 5 (2016)
- Pages: 1034-1039
- Section: Article
- URL: https://journals.rcsi.science/1027-4510/article/view/189874
- DOI: https://doi.org/10.1134/S1027451016050360
- ID: 189874
Cite item
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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