Citation: | Liu Xiaoyan, Wu Zhigang, Yang Chao, et al. Flow field analysis and experimental investigation on gust generator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(7): 803-807. (in Chinese) |
[1] Ricci S,Scotti A.Wind tunnel testing of an active controlled wing under gust excitation .AIAA-2008-1727,2008 [2] Silva W A,Vartio E,Shimko A,et al. Development of aeroservoelastic analytical models and gust load alleviation control laws of a sensorcraft wind-tunnel model using measured data .AIAA-2006-1935,2006 [3] Buell D A.An experimental investigation of the velocity fluctuations behind oscillating vanes .NASA TN D-5543,1969 [4] Grissom D L,Devenport W J.Development and testing of a deterministic disturbance generator .AIAA-2004-2956,2004 [5] Wang Z J.Vortex shedding and frequency selection in flapping flight[J].J Fluid Mech,2000,410:323-341 [6] 宋红军,王肇,尹协振.二维翼型非定常运动数值模拟[J].水动力学研究与进展,2004,19(A):896-903 Song Hongjun,Wang Zhao,Yin Xiezhen.Numerical simulation on unsteady motion of 2D airfoil[J].Journal of Hydrodynamics,2004,19(A):896-903(in Chinese) [7] Anderson J M,Streitlien K,Barrett D S,et al.Oscillating foils of high propulsive efficiency[J].J Fluid Mech,1998,360:41-72
|