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A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio

机译：利用有限长宽比机翼的跨音速相似律对矩形机翼的实验零升阻力与对称NaCa 65系列翼型截面的相关性

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Danforth, Edward C B;
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年度 1951
页码 1-22
总页数 22
原文格式 PDF
正文语种 eng
中图分类工业技术;
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A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio

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