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Pressure distributions at Mach numbers from 0.6 to 1.9 measured in free flight on a parabolic body of revolution with sharply convergent afterbody

机译：马赫数为0.6至1.9的压力分布在自由飞行中测量，在抛物线的旋转体上具有急剧收敛的后体

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作者
Stoney, William E , Jr;
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年度 1952
页码 1-36
总页数 36
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Numerical modeling of the pressure distribution on the axisymmetric body surface at the supersonic freestream interaction with a transversely blown gas jet [J] . V.A. Kislovskiy, V.I. Zvegintsev Thermophysics and Aeromechanics . 2019,第1期

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3. Heat Transfer Measurements on the Afterbody of Spheres in Hypersonic Free-Flight in Air and Carbon Dioxide [C] . Michael C. Wilder, David W. Bogdanoff, David A. Saunders AIAA thermophysics conference . 2015

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4. An experimental investigation of the pressure distributions on five bodies of revolution at Mach numbers of 2.45 and 3.19 [O] . Marson G. B., Socha W., Keates R. E. 1954

机译：马赫数为2.45和3.19的五个公转体上压力分布的实验研究

Pressure distributions at Mach numbers from 0.6 to 1.9 measured in free flight on a parabolic body of revolution with sharply convergent afterbody

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