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


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

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

补充文件

附件文件
动作
1. JATS XML

版权所有 © Pleiades Publishing, Ltd., 2016