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Leading Edge Vortex Flaps on Moderate Sweep Wings- UCAV, Flow Improvement at High Lift

机译：中度扫掠机翼上的前沿涡流襟翼-UCAV，高升程时的流量改善

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《AIAA Aerospace Sciences Meeting and Exhibit》|2007年|P.1-17|共17页
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R. Nangia; M. Palmer;
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中图分类航空;
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专利

1. Leading-edge flow criticality as a governing factor in leading-edge vortex initiation in unsteady airfoil flows [J] . Ramesh Kiran, Granlund Kenneth, Ol Michael V., Theoretical and Computational Fluid Dynamics . 2018,第2期

机译：作为非定常翼型流动的前沿涡旋启动中的主导流量临界。
2. Aerodynamic forces and flow structures of the leading edge vortex on a flapping wing considering ground effect [J] . Van Truong T., Byun D., Kim M.J., Bioinspiration & biomimetics . 2013,第3期

机译：考虑地面效应的襟翼前缘涡流的空气动力和流动结构
3. Force production and flow structure of the leading edge vortex on flapping wings at high and low Reynolds numbers [J] . Birch JM, Dickson WB, Dickinson MH The Journal of Experimental Biology . 2004,第7期

机译：雷诺数高低时襟翼上前缘涡流的力产生和流动结构
4. Leading Edge Vortex Flaps on Moderate Sweep Wings- UCAV, Flow Improvement at High Lift [C] . AIAA Aerospace Sciences Meeting and Exhibit . 2007

机译：在适度扫描翅膀上的前沿涡旋襟翼，高升力的流动改善
5. Static and dynamic leading-edge-flap effects on the vortex lift of a delta wing [D] . Karagounis, Thales 1997

机译：静态和动态前缘襟翼对三角翼涡旋升力的影响
6. The role of the leading edge vortex in lift augmentation of steadily revolving wings: a change in perspective [O] . Mostafa R. A. Nabawy, William J. Crowther 2017

机译：前缘涡旋在稳定旋转机翼升力增强中的作用：视角的改变
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
8. THE USE OF A LEADING-EDGE AREA-SUCTION FLAP AND LEADING-EDGE MODIFICATIONS TO IMPROVE THE HIGH-LIFT CHARACTERISTICS OF AN AIRPLANE MODEL WITH A WING OF 45° SWEEP AND ASPECT RATIO 2.8 [R] . David G. Koenig, Kiyoshi Aoyagi 1957

机译：采用引导边缘区域吸引式襟翼和前沿修正来改善飞机模型的高升特性，翼径为45°，宽度为2.8°

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