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Experimental Investigations of the Two-Dimensional Limitations on Maximum Lift Coefficient Using Small Split Flaps, a Blowing Jet, and Boundary Layer Control

机译：利用小分裂襟翼，吹气射流和边界层控制对最大升力系数二维极限的实验研究

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作者
Kittredge, C. P.; Knowlton, M. P.; Willauer, W. R.;
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年度 1958
页码 p.1-51
总页数 51
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Lift; Split flaps; Boundary layer control; Two dimensional; Jet flow; Interactions; Coefficients; Suction slots; Coanda effect; Wake; Mixing; Limitations;

机译：提升;分裂襟翼;边界层控制;二维;射流;相互作用;系数;吸力槽;柯恩达效应;尾流;混合;限制;

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3. Application of a Synthetic Jet to Control Boundary Layer Separation under Ultra-High-Lift Turbine Pressure Distribution [J] . Davide Lengani, Daniele Simoni, Marina Ubaldi, Flow, Turbulence and Combustion . 2011,第4期

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5. An investigation of the effect of a varying boundary layer on the lift and drag coefficients of a circular cylinder next to a solid boundary. [D] . Chavez, Manuel. 1969

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Experimental Investigations of the Two-Dimensional Limitations on Maximum Lift Coefficient Using Small Split Flaps, a Blowing Jet, and Boundary Layer Control

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