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A preliminary theoretical study of helicopter-blade flutter involving dependence upon coning angle and pitch setting

机译：直升机叶片颤振的初步理论研究，包括对锥角和俯仰设置的依赖

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作者
Coleman, Robert P;
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年度 1946
页码 1-11
总页数 11
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
FLUTTER - PROPELLERS, HELICOPTER;

机译：FLUTTER - 螺旋桨，直升机;

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A preliminary theoretical study of helicopter-blade flutter involving dependence upon coning angle and pitch setting

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