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Characteristics of a 40 degree cone for measuring Mach number, total pressure, and flow angles at supersonic speeds

机译：40度锥体的特征，用于测量超音速下的马赫数，总压力和流动角度

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Centolanzi, Frank J;
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年度 1957
页码 1-37
总页数 37
原文格式 PDF
正文语种 eng
中图分类工业技术;
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入库时间 2022-08-29 11:19:17

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2. Numerical Study of Flow Angles and Mach Number Measurement Using the Surface Pressure of a Supersonic Aircraft with Nose Cone [J] . Katsuyoshi Fukiba, Nobuyuki Tsuboi, Hiroaki Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2012,第2期

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6. First Approximation of Pressure Distribution on Curved Profiles at Supersonic Speeds [O] . T. Y. Thomas 1949

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Characteristics of a 40 degree cone for measuring Mach number, total pressure, and flow angles at supersonic speeds

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