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Rocket-model investigation of hinge-moments on a trailing-edge control on a 52.5 degree swept wing between Mach numbers of 0.70 and 1.80

机译：在马赫数0.70和1.80之间的52.5度后掠翼上的后缘控制上的铰链力矩的火箭模型研究

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作者
Martz, C William;
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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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3. Linear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2 [J] . Kosinov A. D., Kolosov G. L., Semionov N. V., Physics of fluids . 2016,第6期

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Rocket-model investigation of hinge-moments on a trailing-edge control on a 52.5 degree swept wing between Mach numbers of 0.70 and 1.80

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