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A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock

机译：飞行研究边界层的形状和厚度对存在冲击时压力分布的影响

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Harrin, Eziaslav N;
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年度 1952
页码 1-14
总页数 14
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Experimental investigation on the influence of boundary layer thickness on the base pressure and near-wake flow features of an axisymmetric blunt-based body [J] . Mariotti A., Buresti G. Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2013,第11期

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A flight investigation of the effect of shape and thickness of the boundary layer on the pressure distribution in the presence of shock

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