Design of Wing- Body Configurations to Delay the Onset of Vortex Asymmetry

机译：延缓涡旋不对称性发作的机翼结构设计

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来源
《24th Applied Aerodynamics Conference》|2006年|P.1-22|共22页
会议地点 San Francisco CA(US)
作者
J. Cai; H. Tsai; S. Luo; F. Liu;
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作者单位

Temasek Laboratories, National University of Singapore, Kent Ridge Crescent, Singapore;

Temasek Laboratories, National University of Singapore, Kent Ridge Crescent, Singapore;

Department of Mechanical and Aerospace Engineering, University of California, Irvine, CA;

Department of Mechanical and Aerospace Engineering, University of California, Irvine, CA;

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中图分类空气动力学;
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4. Design of Wing- Body Configurations to Delay the Onset of Vortex Asymmetry [C] . Applied Aerodynamics Conference . 2006

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8. Free-Fall Measurements at Transonic Velocities of the Drag of a Wing- Body Configuration Consisting of a 45 deg Swept-Back Wing Mounted Forward of the Maximum Diameter on a Body of Fineness Ratio 12 [R] . Mathews, C. W., Thompson, J. R. 1947

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Design of Wing- Body Configurations to Delay the Onset of Vortex Asymmetry

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