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Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of a spoiler-slot-deflector control located at two spanwise positions

机译：翼前缘襟翼和弦杆延伸对位于两个翼展位置的扰流板 - 槽 - 偏转器控制器的高亚音速控制特性的影响

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Thompson, Robert F; Taylor, Robert T;
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年度 1954
页码 1-80
总页数 80
原文格式 PDF
正文语种 eng
中图分类工业技术;
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专利

1. Control of vortical structures on a flapping wing via a sinusoidal leading-edge [J] . Ozen CA, Rockwell D Physics of fluids . 2010,第2期

机译：通过正弦前缘控制襟翼上的旋涡结构
2. APS -70th Annual Meeting of the APS Division of Fluid Dynamics- Event - Effect of controlled spanwise bending on the stability of the leading-edge vortex [J] . Samik Bhattacharya, Tyler Scofield Bulletin of the American Physical Society . 2017,第14期

机译：APS-流体动力学APS部门第70届年会-事件-受控展向弯曲对前沿涡流稳定性的影响
3. Effect of leading-edge plate controlling on subsonic cavity [J] . International Journal of Modern Physics, B. Condensed Matter Physics, Statistical Physics, Applied Physics . 2020,第14a16期

机译：前缘板控制对亚腔的影响
4. Control of Double-Delta-Wing Vortex by Micro Leading-Edge Flap [C] . Myong H. Sohn, Hyoung S. Chung, Jo W. Chang AIAA Applied Aerodynamics Conference . 2007

机译：通过微型前沿襟翼控制双δ-翼涡流
5. Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight. [D] . Colmenares, David. 2017

机译：能够控制飞行的共振扑翼式微型飞行器的设计与控制。
6. Petiolate wings: effects on the leading-edge vortex in flapping flight [O] . Nathan Phillips, Kevin Knowles, Richard J. Bomphrey 2017

机译：叶柄翅膀：扑翼飞行中对前沿涡旋的影响
7. Formation of the leading-edge vortex and spanwise flow on an insect-like flapping-wing throughout a flapping half cycle [O] . Phillips N., Knowles K. 2013

机译：在整个拍打半周期中，前涡旋的形成和翼展流在像昆虫一样的拍打翼上

Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of a spoiler-slot-deflector control located at two spanwise positions

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