[1] Smith BL, Glezer A. The formation and evolution of synthetic jets. Physics of Fluids, 1998, 10(9): 2281-2297
[2] Durrani D, Haider BA. Study of stall delay over a generic airfoil using synthetic jet actuator. AIAA-2011-943, 2011
[3] Rumsey TB, Gatski WL. Summary of the 2004 CFD validation workshop on synthetic jets and turbulent separation control. AIAA 2004-2217, 2004
[4] Seifert A, Darabi A, Wygnanski I. Delay of airfoil stall by periodic excitation. AIAA J, 1999, 33 (4): 691-707
[5] Greenblatt D, Wygnanski IJ. The control of flow separation by period excitation. Progress in Aerospace Sciences, 2000, 36(7): 487-545
[6] Gilarranz JL, Train LW, Rediniotis OK. A new class of synthetic jet actuators: Part II: Application to flow separation control. Journal of Fluids Engineering, 2005, 127(2): 377-387
[7] He YY, Cary AW, Peters DA. Parametric and dynamic modeling for synthetic jet control of a post-stall airfoil. AIAA-2001-733; 2001
[8] Hassan AA. A two-point active flow control strategy for improved airfoil stall/post stall aerodynamics. AIAA-2006-99, 2006
[9] 韩忠华, 宋文萍, 乔志德. YLSG107高升力翼型主动流动控制的数值模拟. 计算物理, 2009, 26(6): 837-841 (Han Zhonghua, Song Wenping, Qiao Zhide. Numerical simulation of active stall control on high-lift airfoil. Chinese Journal of Computational Physics, 2009, 26(6): 837-841 (in Chinese))
[10] 张攀峰, 王晋军. 孔口倾斜角对合成射流控制翼型流动分离的影响. 兵工学报, 2009, 30(12): 1658-1662 (Zhang Panfeng, Wang Jinjun. Effect of orifice inclined angle on flow control of the stalled airfoil with synthetic jet actuator. Acta Armament Arii, 2009, 30(12): 1658-1662 (in Chinese))
[11] 刘峰, 邹建锋, 郑耀. 合成射流物理参数对控制翼型流动分离的影响. 浙江大学学报(工学版), 2013, 47(1): 147-153 (Liu Feng, Zou Jianfeng, Zheng Yao. Effect of synthetic jets physical parameters on flow separation control over airfoil. Journal of Zhejiang University (Engineering Science), 2013, 47(1): 147-153 (in Chinese)) |