ENGINEERING MODELING OF A SPATIALLY INHOMOGENEOUS TRANSITION TO TURBULENCE IN A SWEPT-WING BOUNDARY LAYER

IF 0.6 4区 工程技术 Q4 MECHANICS Journal of Applied Mechanics and Technical Physics Pub Date : 2025-04-18 DOI:10.1134/S0021894424060117
A.V. Boiko, S.V. Kirilovskiy, T.V. Poplavskaya
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引用次数: 0

Abstract

Results of a methodical study aimed at modeling a spatially inhomogeneous transition line are reported. The results are obtained by an in-house software module for the CFD package and an in-house program for predicting the laminar-turbulent transition based on the \(\mathrm{e}^N\)-method. Numerical simulations are performed for a hybrid laminar-turbulent transition, where the regular and bypass transition scenarios take place in different regions of the flow in the swept-wing boundary layer.

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后掠翼边界层空间非均匀过渡到湍流的工程模拟
结果的系统研究旨在模拟一个空间不均匀的过渡线报告。计算结果由内部的CFD软件包软件模块和内部的基于\(\mathrm{e}^N\) -方法的层流-湍流过渡预测程序获得。数值模拟了后掠翼边界层内不同区域发生的常规和旁路混合层流转捩。
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来源期刊
CiteScore
1.20
自引率
16.70%
发文量
43
审稿时长
4-8 weeks
期刊介绍: Journal of Applied Mechanics and Technical Physics is a journal published in collaboration with the Siberian Branch of the Russian Academy of Sciences. The Journal presents papers on fluid mechanics and applied physics. Each issue contains valuable contributions on hypersonic flows; boundary layer theory; turbulence and hydrodynamic stability; free boundary flows; plasma physics; shock waves; explosives and detonation processes; combustion theory; multiphase flows; heat and mass transfer; composite materials and thermal properties of new materials, plasticity, creep, and failure.
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