Mathematical model of the supersonic heterogeneous flow incident on a flat obstacle
- 作者: Nikitin P.V.1, Borisov S.A.1, Dobrovolskiy S.V.1, Glukhovskaya Y.I.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 10, 编号 5 (2016)
- 页面: 1034-1039
- 栏目: Article
- URL: https://journals.rcsi.science/1027-4510/article/view/189874
- DOI: https://doi.org/10.1134/S1027451016050360
- ID: 189874
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详细
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.
作者简介
P. Nikitin
Moscow Aviation Institute (National Research University)
Email: gljul@bk.ru
俄罗斯联邦, Moscow, 125993
S. Borisov
Moscow Aviation Institute (National Research University)
Email: gljul@bk.ru
俄罗斯联邦, Moscow, 125993
S. Dobrovolskiy
Moscow Aviation Institute (National Research University)
Email: gljul@bk.ru
俄罗斯联邦, Moscow, 125993
Yu. Glukhovskaya
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: gljul@bk.ru
俄罗斯联邦, Moscow, 125993
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