Rotor/empennage unsteady aerodynamic interaction with unsteady panel/viscous vortex particle hybrid method

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作者：
School of Mechanical and Power Engineering, Nanjing University of Technology, Nanjing 211816, China [1 ]
不详 [2 ]
不详 [3 ]
不详 [4 ]
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来源：
Hangkong Xuebao | / 3卷 / 643-656期
关键词：
Helicopter rotors;
D O I：
10.7527/S1000-6893.2013.0324
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