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An investigation at low speed of a 51.3 degrees sweptback semispan wing with a raked tip and with 16.7-percent-chord ailerons having three spans and three trailing-edge angles

机译：一个51.3度后掠半翼机翼的低速研究，带有倾斜的尖端和16.7％的弦副翼具有三个跨度和三个后缘角

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作者
Schneiter, Leslie E; Fischel, Jack;
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年度 1948
页码 1-57
总页数 57
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Experimental investigation into wing span and angle-of-attack effects on sub-scale race car wing/wheel interaction aerodynamics [J] . S. Diasinos, A. Gatto Experiments in Fluids . 2008,第3期

机译：机翼跨度和攻角对小尺度赛车机翼/车轮相互作用空气动力学影响的实验研究
2. Experimental investigation into wing span and angle-of-attack effects on sub-scale race car wing/wheel interaction aerodynamics [J] . Diasinos S, Gatto A Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2008,第3期

机译：翼展和攻角对小型赛车翼/轮相互作用空气动力学影响的实验研究
3. Numerical simulation of flow over delta wing with trailing-edge jet at high angle of attack [J] . Z. K. Zhang, H. S. Tang International Journal for Numerical Methods in Engineering . 2004,第15期

机译：高攻角后缘射流在三角翼上流动的数值模拟
4. Interaction of a Finite-Span Synthetic-Jet and a Cross-Flow over a Sweptback Finite Wing [C] . Joseph Vasile, Michael Amitay AIAA flow control conference . 2012

机译：有限跨度合成射流和后掠有限翼上的横流相互作用
5. Investigation of three-dimensional flow structure on maneuvering finite-span wings [D] . Yilmaz, Turgut Oruc 2012

机译：机动有限跨机翼三维流动结构研究
6. Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4 [O] . Emslie K., Hosking L., Marshall W. S. D. 1953

机译：纵横比为4的45度后掠无锥翼边界层流动的一些实验

An investigation at low speed of a 51.3 degrees sweptback semispan wing with a raked tip and with 16.7-percent-chord ailerons having three spans and three trailing-edge angles

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