Numerical Simulation of the Receptivity of a Supersonic Boundary Layer to Acoustic Disturbances in Compression and Rarefaction Flows

被引：1
作者：
Egorov, I. V. [1 ,2 ]
Palchekovskaya, N. V. [1 ,2 ]
机构：
[1] Moscow Inst Phys & Technol, Dolgoprudnyi, Moscow Oblast, Russia
[2] Cent Aerohydrodynam Inst, Zhukovskii, Moscow Oblast, Russia
来源：
DOKLADY PHYSICS | 2021年 / 66卷 / 03期
基金：
俄罗斯科学基金会;
关键词：
boundary layer; receptivity; acoustic disturbances; numerical simulation; Navier-Stokes equations;
D O I：
10.1134/S1028335821030022
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The receptivity of a boundary layer on a flat plate to acoustic disturbances in an incoming supersonic gas flow is studied numerically. Angles of attack are considered, at which shock waves and a rarefaction fanlike spread are generated in the flow field. The peculiarities of the interaction of these structures with acoustic waves have been studied, and regularities in the origin of the boundary layer instability region have been obtained.
引用
收藏
页码：76 / 79
页数：4
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