On computing the location of laminar-turbulent transition in compressible boundary layers

被引:19
|
作者
Boiko, Andrey V. [1 ]
Demyanko, Kirill V. [2 ]
Nechepurenko, Yuri M. [2 ]
机构
[1] Russian Acad Sci, Siberian Branch, Khristianovich Inst Theoret & Appl Mech, Novosibirsk 630090, Russia
[2] Russian Acad Sci, Inst Numer Math, Moscow 119333, Russia
基金
俄罗斯科学基金会; 俄罗斯基础研究基金会;
关键词
Compressible flows; laminar-turbulent transition; evolution equations of small disturbances; e(N)-method;
D O I
10.1515/rnam-2017-0001
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
Evolution equations of small disturbances aimed to compute the location of a laminar-turbulent transition in boundary layers by the e(N)-method taking into account the compressibility and heat transfer are described and justified for aerodynamic applications. The results of computation of N-factors and transition locations with the use of locally-parallel flow assumption for a flat plate exposed to supersonic flow at zero angle of attack are given. The results agree well with known numerical and experimental data.
引用
收藏
页码:1 / 12
页数:12
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