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Trim Requirements and Static-Stability Derivatives from a Wind-Tunnel Investigation of a Lifting Rotor in Transition

机译：转换中提升转子风洞研究中的修剪要求和静稳定导数

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作者
Jenkins, J. L.;
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年度 1965
页码 1-3
总页数 3
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aerodynamic stability ; Wind tunnel tests ; Rotary wing aircraft ; Lift;

机译：空气动力学稳定性;风洞试验;旋翼飞机;升力;

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2. Method for eliminating aerodynamic lift vibration of rigid rotor helicopters based on the novel sine-trim model [J] . Aerospace science and technology . 2020,第Mara期

机译：基于新型正弦修剪模型的刚性旋翼直升机气动升力振动消除方法
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8. Trim requirements and static-stability derivatives from a wind-tunnel investigation of a lifting rotor in transition [R] . Jenkins, J. L., Jr. 1965

机译：通过对过渡中的提升转子的风洞调查修剪要求和静态稳定性导数

Trim Requirements and Static-Stability Derivatives from a Wind-Tunnel Investigation of a Lifting Rotor in Transition

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