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Investigation of the flow over flying wing surface with three-dimensional roughness placed on the leading edge

机译：用三维粗糙度放置在前缘的飞行翼面流动的调查

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V. S. Kaprilevskaya; A. M. Pavlenko; V. V. Kozlov;
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1. Stationary crossflow vortices near the leading edge of three-dimensional boundary layers: the role of non-parallelism and excitation by surface roughness [J] . Butler Adam, Wu Xuesong Journal of Fluid Mechanics . 2018,第期

机译：静止的十字流涡流附近的三维边界层的前缘：表面粗糙度的非平行和激发的作用
2. A CFD Study on Leading Edge Wing Surface Modification of a Low Aspect Ratio Flying wing to Improve Lift Performance [J] . Ramprasadh C., Devanandh V. International journal of micro air vehicles . 2015,第3期

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3. AVF-183 diamond wing flow field characteristics Part 1: Varying leading-edge roughness and the effects on flow separation onset [J] . Hoevelmann Andreas, Knoth Florian, Breitsamter Christian Aerospace science and technology . 2016,第octa期

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5. Flow visualization and three-dimensional characteristics of the leading edge vortex on a hovering model hummingbird wing. [D] . Swanton, Erik William M. 2008

机译：悬停模型蜂鸟机翼上的流动可视化和前缘涡旋的三维特征。
6. The leading-edge vortex of swift wing-shaped delta wings [O] . Rowan Eveline Muir, Abel Arredondo-Galeana, Ignazio Maria Viola 2017

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7. Experimental investigation of leading-edge roughness effects on stationary crossflow instability of a swept wing [O] . Soltani M.R., Masdari M., Damghani H. 2013

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8. The effect of span and deflection of split flaps and leading-edge roughness on the longitudinal stability and gliding characteristics of a 42 degree sweptback wing equipped with leading-edge flaps [R] . Pratt, George L, Bollech, Thomas V 1949

机译：分裂襟翼的跨度和挠度以及前缘粗糙度对配备有前缘襟翼的42度后掠翼的纵向稳定性和滑行特性的影响

Investigation of the flow over flying wing surface with three-dimensional roughness placed on the leading edge

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