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Investigation of a ramp-type inlet designed for improved angle-of-attack performance at Mach number 2.0

机译：研究了一种斜坡式进气口，设计用于改善马赫数为2.0的迎角性能

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Wise, G A; Campbell, R C;
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年度 1955
页码 1-16
总页数 16
原文格式 PDF
正文语种 eng
中图分类工业技术;
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Investigation of a ramp-type inlet designed for improved angle-of-attack performance at Mach number 2.0

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