Numerical simulation of a laminar-turbulent flow past a swept wing under the action of a blowing or suction source

被引：0
|
作者：
Boiko, A. V. [1 ]
Kirilovskiy, S. V. [1 ]
Poplavskaya, T. V. [1 ]
机构：
[1] RAS, Khristianovich Inst Theoret & Appl Mech, SB, Novosibirsk, Russia
来源：
THERMOPHYSICS AND AEROMECHANICS | 2024年 / 31卷 / 02期
基金：
俄罗斯科学基金会;
关键词：
laminar-turbulent flow; subsonic flows; e(N)-method of determining the transition position; numerical simulation; TRANSITION;
D O I：
10.1134/S0869864324020057
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A method and results of computing a laminar-turbulent flow past a swept wing under a control action generated by a source of blowing or suction from the model surface are presented. Pioneering results on the influence of three-dimensional blowing and suction sources on stability of the boundary layer on a swept wing and distributions of N-factors of various mechanisms of the laminar-turbulent transition aimed at changing its position are obtained by using the LOTRAN 3 software package.
引用
收藏
页码：245 / 254
页数：10
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