Hypersonic boundary layer transition and control

被引：2
|
作者：
Maslov, A. A. [1 ]
Poplavskaya, T. [2 ]
Bountin, D. A. [2 ]
机构：
[1] RAS, Khristianovich Inst Theoret & Appl Mech, SB, ITAM, Inst Skaya Str 4-1, Novosibirsk, Russia
[2] Novosibirsk State Univ, ITAM, Novosibirsk, Russia
来源：
SEVENTH IUTAM SYMPOSIUM ON LAMINAR-TURBULENT TRANSITION | 2010年 / 18卷
基金：
俄罗斯基础研究基金会;
关键词：
SHOCK LAYER; FLAT-PLATE; DISTURBANCES; SURFACE; WAVES;
D O I：
10.1007/978-90-481-3723-7_3
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
In the present paper an overview of the recent studies of a hypersonic lam mar boundary layer and shock layer receptivity and stability are presented. Main attention is paid to investigations of nonlinear wave interaction New active and passive methods or hypersonic stability control are described too
引用
收藏
页码：19 / +
页数：2
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