EFFECT OF THE BOUNDARY LAYER ON THE BASE PRESSURE IN A TWO-DIMENSIONAL FLOW WITH A MACH NUMBER M = 5

M. G. Ktalkherman; V. M. Malkov

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EFFECT OF THE BOUNDARY LAYER ON THE BASE PRESSURE IN A TWO-DIMENSIONAL FLOW WITH A MACH NUMBER M = 5

机译：马赫数M = 5的二维流中边界层对基压力的影响

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摘要

New data on the base pressure in a two-dimensional flow with a Mach number M = 5 are obtained for a wide range of variation of the normalized boundary-layer thickness in the flow-separation cross section. The test results are compared with Tanner's theory, and a conclusion is made that this numerical model has to be corrected.

机译：对于分流截面中归一化边界层厚度的较大变化范围，获得了马赫数M = 5的二维流中基本压力的新数据。将测试结果与Tanner理论进行了比较，得出结论，该数值模型必须进行校正。

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来源
《Journal of Applied Mechanics and Technical Physics》 |2005年第3期|p.324-328|共5页
作者
M. G. Ktalkherman; V. M. Malkov;
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作者单位

Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk 630090;

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原文格式 PDF
正文语种 eng
中图分类应用力学;
关键词
supersonic flow; turbulent boundary layer; base pressure;

机译：超音速流动;湍流边界层;基础压力;

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EFFECT OF THE BOUNDARY LAYER ON THE BASE PRESSURE IN A TWO-DIMENSIONAL FLOW WITH A MACH NUMBER M = 5

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