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Some effects of aeroelasticity on the rolling effectiveness of a 10-percent-scale model of the McDonnell F-101A airplane wing at Mach numbers from 0.5 to 1.2

机译：气动弹性对麦克唐纳F-101a飞机机翼10％比例模型在马赫数为0.5到1.2时的滚动效率的影响

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English, Roland D;
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年度 1955
页码 1-13
总页数 13
原文格式 PDF
正文语种 eng
中图分类工业技术;
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3. Unsteady Wing-Body Aerodynamics for Aeroelastic Applications at Mach One [J] . P. C. Chen, D. D. Liu AIAA Journal . 2006,第8期

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5. Modeling the rolling moment on the 65-degree delta wing for rolling motions at high angle of attack. [D] . Myatt, James Harold. 1997

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8. Rocket-powered-model investigation of the effects of aeroelasticity on the rolling effectiveness of an 8.06-percent-scale McDonnell F3H-1 airplane wing at Mach numbers from 0.5 to 1.4 : TED No. NACA DE 351 [R] . English, Roland D 1954

机译：火箭动力模型研究气动弹性对8.06％规模的麦克唐纳F3H-1飞机机翼在马赫数为0.5到1.4时的滚动效果的影响：TED No. NaCa DE 351

Some effects of aeroelasticity on the rolling effectiveness of a 10-percent-scale model of the McDonnell F-101A airplane wing at Mach numbers from 0.5 to 1.2

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