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引用次数: 0
摘要
本文介绍了在由模型表面的吹力或吸力源产生的控制作用下计算掠过机翼的层流-湍流的方法和结果。通过使用 LOTRAN 3 软件包，获得了三维吹气源和吸力源对后掠翼边界层稳定性影响的开创性结果，以及旨在改变其位置的层流-湍流过渡的各种机制的 N 因子分布。
Numerical simulation of a laminar-turbulent flow past a swept wing under the action of a blowing or suction source
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.
期刊介绍：
The journal Thermophysics and Aeromechanics publishes original reports, reviews, and discussions on the following topics: hydrogasdynamics, heat and mass transfer, turbulence, means and methods of aero- and thermophysical experiment, physics of low-temperature plasma, and physical and technical problems of energetics. These topics are the prior fields of investigation at the Institute of Thermophysics and the Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences (SB RAS), which are the founders of the journal along with SB RAS. This publication promotes an exchange of information between the researchers of Russia and the international scientific community.
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