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An experimental investigation of the effects of two inlet boundary layer conditions on the performance of a 12 deg conical diffuser operating at subsonic Mach numbers up to Mach number 1.0

机译：两个入口边界层条件对12度锥形扩散器性能影响的实验研究，该扩散器工作在马赫数为1.0的亚音速马赫数

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作者
Little, B. H., Jr.;
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年度 1951
页码 1-96
总页数 96
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BOUNDARY CONDITIONS; BOUNDARY LAYERS; CONICAL FLOW; DIFFUSERS; ENGINE INLETS; AERODYNAMIC CONFIGURATIONS; FREE FLOW; MATHEMATICAL MODELS; STATIC PRESSURE;

机译：边界条件;边界层;圆锥形流动;扩散器;发动机进气;空气动力学配置;自由流动;数学模型;静压力;

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9. High-Subsonic Performance Characteristics and Boundary-Layer Investigations of a 12 deg 10-Inch-Inlet-Diameter Conical Diffuser [R] . 1950

机译：高亚音速性能特点和一个12度10英寸的入口直径渐扩的边界层调查

An experimental investigation of the effects of two inlet boundary layer conditions on the performance of a 12 deg conical diffuser operating at subsonic Mach numbers up to Mach number 1.0

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