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Interaction of a Shock Wave with a Turbulent Boundary Layer on a Heated Surface

机译:激波与受热表面上湍流边界层的相互作用

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摘要

The interaction of a shock wave with a turbulent boundary layer has been studied. A stream has been diagnosed using non-invasive visualization (schlieren method). During the investigation the effect of surface heating on the length of boundary layer separation has been studied. It has been discovered that during surface heating the dependence of the length of separation on the temperature ratio is approximated using a linear law.
机译:研究了冲击波与湍流边界层的相互作用。使用非侵入性可视化(schlieren方法)已诊断出流。在研究过程中,研究了表面加热对边界层分离长度的影响。已经发现,在表面加热期间,使用线性定律来近似分离长度对温度比的依赖性。

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