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Dynamic stability investigation of two right circular cylinders in axial free-flight at Mach numbers from 0.4 to 1.7 : fineness-ratio-2.56 cylinder and fineness-ratio-4.0 cylinder with flared afterbody

机译：轴向自由飞行中两个直径圆柱体在马赫数为0.4到1.7时的动态稳定性研究：细度比为2.56的圆柱体和细度比为4.0的带有扩口后体的圆柱体

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Mcfall, John C , Jr;
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年度 1957
页码 1-45
总页数 45
原文格式 PDF
正文语种 eng
中图分类工业技术;
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机译：对于不同的气缸间距s和迎角φ，对垂直浸入湍流边界层的直径为d的两个圆柱上的压力分布进行测量。作用在气缸上的阻力和提升力的特性分为三个区域：1）0°＜__ 〜φ ＜__ 〜30°，2）30°＜__ 〜φ ＜__ 〜120°和3） 120°＜__ 〜φ ＜__ 〜180°除以两条零升力线。而且，发现除了上游气缸的尾流区域的影响之外，对于s / d＞ __〜4，两个气缸之间的干扰几乎可以忽略。

Dynamic stability investigation of two right circular cylinders in axial free-flight at Mach numbers from 0.4 to 1.7 : fineness-ratio-2.56 cylinder and fineness-ratio-4.0 cylinder with flared afterbody

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