| [1] Hall R M. Forebody and missile side forces and the time analogy, AIAA-1987-0327[R]. Reston: AIAA, 1987.[2] Lamont P J. Pressure around an inclined ogive cylinder with laminar, transitional, or turbulent separation[J]. AIAA Journal, 1982, 20(11): 1492-1496.[3] Ericsson L E. Sources of high alpha vortex asymmetry at zero sideslip[J]. Journal of Aircraft, 1992, 29(6): 1086-1090.[4] Zhang H X, Ran Z. On the structural stability of the flows over slenders at angle of attack[J]. Acta Aerodynamica Sinica, 1997, 15(1): 20-26 (in Chinese). 张涵信, 冉政. 细长锥体有攻角绕流对称流态到非对称流态的结构稳定性研究[J]. 空气动力学学报, 1997, 15(1): 20-26.[5] Liu P Q, Deng X Y, Kong F M. Experimental investigation of asymmetry vortex unsteadiness over slender cylinders[J]. Experiments and Measurements in Fluid Mechanics, 2002, 16(4): 39-46 (in Chinese). 刘沛清, 邓学蓥, 孔繁美. 绕细长旋成体非对称涡非定常性的实验研究[J]. 流体力学实验与测量, 2002, 16(4): 39-46.[6] Wang Y K, Wei Z F, Deng X Y. An experimental study on forebody vortex flow control technique using combined perturbation[J]. Chinese Journal of Theoretical and Applied Mechanics, 2007, 39(4): 433-441 (in Chinese). 王延奎, 魏占峰, 邓学蓥. 飞机大迎角非对称涡组合扰动主动控制研究[J]. 力学学报, 2007, 39(4): 433-441.[7] Shah G H, Granda J N. Application of forebody strakes for directional stability and control of transport aircraft, AIAA-1998-4448[R]. Reston: AIAA, 1998.[8] Yanta W J, Wardlaw A B. Flow field about and forces on slender bordies at high angles of attack[J]. AIAA Journal, 1981, 19(3): 296-302.[9] Cobleigh B R. High angle of attack yawing moment asymmetry of the X-31 aircraft from flight test, NASA CR 186030[R]. Washington, D.C.: NASA, 1994.[10] Murri D G, Shah G H, Dicarlo D J. Actuated forebody strake controls for the F-18 high alpha research vehicle [J]. Journal of Aircraft, 1995, 32(3): 555-562.[11] Fisher D F, Murri D G. Forebody flow visualization on the F-18 harv with actuated forebody strakes, NASA TM 206556[R]. Washington, D.C.: NASA, 1998.[12] Roos E W. Microblowing: an effective, efficient method of vortex asymmetry management, AIAA-2000-4416 [R]. Reston: AIAA, 2000.[13] Takahara Y, Rock S M. Nonlinear flight control using forebody tangential blowing[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(6): 1157-1166.[14] Williams D. A review of forebody vortex control scenarios, AIAA-1997-1967[R]. Reston: AIAA, 1997.[15] Gu Y S, Ming X. Forebody vortices control using a fast swinging micro-tip-strake at high angles of attack[J]. Acta Aeronautica et Astronautica Sinica, 2003, 24(2): 102-106 (in Chinese). 顾蕴松, 明晓. 大攻角非对称流动的非定常弱扰动控制[J]. 航空学报, 2003, 24(2): 102-106.[16] Gu Y S, Li B B, Cheng K M. High angle of attack asymmetric vortex synthetic jet unsteady small disturbance control device: China. CN102417031A[P]. 2011-10-20 (in Chinese). 顾蕴松, 李斌斌, 程克明. 大攻角非对称涡合成射流非定常小扰动控制装置: 中国. CN102417031A[P]. 2011-10-20. |
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