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Effects of trailing-edge bluntness on the lift, drag, and pitching-moment characteristics of unswept, 45 degree swept, and 45 degree delta wings at Mach numbers of 1.41, 1.62, and 1.96

机译：后缘钝化对未加工，45度扫掠和45度三角翼的升力，阻力和俯仰力矩特性的影响，马赫数为1.41,1.62和1.96

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Goin, Kennith L; Westrick, Gertrude C;
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年度 1953
页码 1-101
总页数 101
原文格式 PDF
正文语种 eng
中图分类工业技术;
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Effects of trailing-edge bluntness on the lift, drag, and pitching-moment characteristics of unswept, 45 degree swept, and 45 degree delta wings at Mach numbers of 1.41, 1.62, and 1.96

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