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Experimental Investigation of Several Wraparound Fins on Bodies of Revolution from Mach 0.3to 1.3.

机译：从0.3到1.3马赫数对旋转体上的环绕翅片的实验研究。

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A wind tunnel test was conducted for several wraparound fin configurations on bodies of revolution at Mach numbers ranging from 0.3to 1.3. Aerodynamic forces and moments were measured by five strain gage balances. A complete listing of the summary data is presented in tabular form.

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作者
dahlke, c. wayne;
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年度 1975
页码 1-810
总页数 810
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
fin stabilized ammunition; aerodynamic forcestube launched; fins; bodies of revolution; wind tunnel tests; roll; aerodynamic stability;

机译：鳍稳定的弹药;空气动力学力量发射;鳍;旋转体;风洞试验;滚动;空气动力学稳定性;

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8. Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3to 1.3. Volume II, [R] . dahlke, c. wayne craft, j. c. 1974

机译：安装在旋转体上的环绕翅片的气动特性及其对0.3~1.3马赫数下导弹静态稳定性的影响。第二卷，

Experimental Investigation of Several Wraparound Fins on Bodies of Revolution from Mach 0.3to 1.3.

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