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Effect of wing flexibility on the damping roll of a notched delta-wing body combination between Mach numbers 0.6 and approximately 2.2 as determined with rocket-propelled models

机译：用火箭推进模型确定的机翼柔度对马赫数0.6和大约2.2之间的缺口三角翼体组合的阻尼滚动的影响

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作者
Bland, William M , Jr;
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年度 1954
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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Effect of wing flexibility on the damping roll of a notched delta-wing body combination between Mach numbers 0.6 and approximately 2.2 as determined with rocket-propelled models

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