Direct numerical simulation of transition to turbulence in a supersonic boundary layer

被引：0
|
作者：
Kudryavtsev, A. N. [1 ]
Khotyanovsky, D. V. [1 ]
机构：
[1] RAS, Khristianovich Inst Theoret & Appl Mech, SB, Novosibirsk, Russia
来源：
THERMOPHYSICS AND AEROMECHANICS | 2015年 / 22卷 / 05期
基金：
俄罗斯科学基金会;
关键词：
direct numerical simulation; laminar-turbulent transition; supersonic boundary layer; FLAT-PLATE; RECEPTIVITY; STABILITY;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Based on full unsteady compressible Navier-Stokes equations a direct numerical simulation of the linear and nonlinear stages of the laminar-turbulent transition in boundary layer of a flate plate at the freestream Mach number M = 2 is carried out.
引用
收藏
页码：559 / 568
页数：10
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