[1] SEIFERT A, DARABI A, WYGNANSKI I J. Delay of airfoil stall by periodic excitation [J]. Journal of Aircraft, 1996, 33(4): 691-698.
[2] GREENBLATT D, WYGNANSKI I J. The control of flow separation by periodic excitation [J]. Progress in Aerospace Sciences, 2000, 36(7): 487-545.
[3] GILARRANZ J L, TRAUB L W, REDINIOTIS O K. Characterization of a compact, highpower synthetic jet actuator for flow separation control [J]. AIAA Paper,2002, 127.
[4] GILARRANZ J L, TRAUB L W, REDINIOTIS O K. A new class of synthetic jet actuators: Part II: application to flow separation control [J]. Journal of Fluids Engineering, 2005, 127(2): 377-387.
[5] SIAUW W L, BONNET J P, TENSI J, et al. Transient dynamics of the flow around a NACA0015 airfoil using fluidic vortex generators [J]. International Journal of Heat and Fluid Flow, 2010, 31(3): 450-459.
[6] DONOVAN J F, KRAL L D, CARY A W. Active flow control applied to an airfoil [J]. AIAA Paper, 1998, 2-10.
[7] DUVIGNEAU R, VISONNEAU M. Simulation and optimization of stall control for an airfoil with a synthetic jet [J]. Aerospace Science and Technology, 2006, 10(4): 279-287.
[8] YOU D, MOIN P. Active control of flow separation over an airfoil using synthetic jets [J]. Journal of Fluids and Structures, 2008, 24(8): 1349-1357.
[9] GEISSLER W. A family of CFD boundary conditions to simulate separation control [J]. Aerospace Science and Technology, 2010, 14(7): 494-504.
[10] REHMAN A, KONTIS K. Synthetic jet control effectiveness on stationary and pitching airfoils [J]. Journal of Aircraft, 2006, 43(6): 1782-1789.
[11] KIM S H, KIM C. Separation control on NACA23012 using synthetic jet [J]. Aerospace Science and Technology, 2009, 13(4/5): 172182.
[12] 顾蕴松,明晓. 应用 PIV 技术研究 “零质量” 射流的非定常流场特性[J]. 实验流体力学, 2005, 19(1): 83-86.
GU Yun-song, MING Xiao. Investigation on the characteristics and structures of unsteady flow field near the zeromass flux jet with PIV [J]. Journal of Experiments in Fluid Mechanics, 2005, 19(1): 83-86.
[13] 洪俊武,陈晓东,张玉伦,等. 主动流动控制技术的初步数值研究[J]. 空气动力学学报, 2005, 23(4): 402-407.
HONG Jun-wu, CHEN Xiao-dong,ZHANG Yu-lun, et al. The primary numerical research of active control technology in flow [J]. Acta Aerodynamica Sinica, 2005, 23(4): 402-407.
[14] 肖中云,牟斌,陈作斌,等. 零质量射流与分离控制的数值模拟[J]. 空气动力学学报, 2006, 24(1): 46-50.
XIAO Zhong-yun, MOU Bin, CHEN Zuo-bin, et al. Compressible simulation of active flow control using synthetic jets [J]. Acta Aerodynamica Sinica, 2006, 24(1): 46-50.
[15] 罗振兵,夏智勋. 合成射流技术及其在流动控制中应用的进展[J]. 力学进展, 2005, 35(2): 221-234.
LUO Zhen-bing, XIA Zhi-xun. Advances in synthetic jet technology and applications in flow control [J]. Advances in Mechanics, 2005, 35(2): 221-234.
[16] 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[J]. 计算物理, 2009, 26(6): 837-841.
HAN Zhong-hua, SONG Wen-ping, QIAO Zhi-de. Numerical simulation of active stall control on highlift airfoil [J]. Chinese Journal of Computational Physics, 2009, 26(6): 837-841.
[17] 韩忠华,乔志德,宋文萍. 合成射流推迟翼型失速的数值模拟[J]. 航空学报, 2007, 28(5): 1040-1046.
HAN Zhong-hua, QIAO Zhi-de, SONG Wen-ping. Numerical simulation of active flow control to airfoil stall using local synthetic jet [J]. Acta Aeronautica Et Astronautica Sinica, 2007, 28(5): 10401046.
[18] 韩忠华,宋文萍,乔志德. OA212 翼型主动流动控制的数值模拟研究[J]. 空气动力学学报, 2009, 27(6): 639-644.
HAN Zhong-hua, SONG Wen-ping, QIAO Zhi-de. Numerical simulation of active dynamic stall control on an OA212 rotor airfoil [J]. Acta Aerodynamica Sinica, 2009, 27(6): 639-644.
[19] 张攀峰,王晋军. 合成射流控制NACA0015翼型大攻角流动分离[J]. 北京航空航天大学学报, 2008, 34(4): 443-446.
ZHANG Pan-feng, WANG Jin-jun. Numerical simulation on flow control of stalled NACA0015 airfoil with synthetic jet actuator in recirculation region [J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(4): 443-446.
[20] 石清,李桦. 零净质量射流的数值模拟[J]. 空气动力学学报, 2011, 29(1): 114-117.
SHI Qing, LI Hua. Numerical simulation of the zero mass jet flow [J]. Acta Aerodynamica Sinica, 2011, 29(1): 114-117. |