[1] KATZ J. Wing/vortex interactions and wing rock[J]. Progress in Aerospace Sciences, 1999, 35(7):727-750.
[2] MALCOLM G N, SKOW A M. Enhanced controllability through vortex manipulation on fighter aircraft at high angles of attack:AIAA-1986-2277[R]. Reston:AIAA, 1986.
[3] ROOS F W. Microblowing for high-angle-of-attack vortex flow control on a fighter aircraft[J]. Journal of Aircraft, 2001, 38(3):454-457.
[4] BERNHARDT J E, WILLIAMS D R. Closed-loop control of forebody flow asymmetry[J]. Journal of Aircraft, 2000, 37(3):491-498.
[5] GAPCYNSKI J P, HASEL L E, COOPER M. A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M=1.59 and angles of attack up to 36 degrees:NACA RM-L52G14a[R]. Washington, D.C.:National Advisory Committee for Aeronautics, 1952.
[6] 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. 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).
[7] HUNT B L. Asymmetric vortex forces and wakes on slender bodies:AIAA-1982-1336[R]. Reston:AIAA, 1982.
[8] ERICSSION L E, BEYERS M E. Fluid mechanics considerations for successful design of forebody flow control:AIAA-2000-2320[R]. Reston:AIAA, 2000.
[9] LAMONT P J, HUNT B L. Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream[J]. Journal of Fluid Mechanics, 1976, 76(8):519-559.
[10] WARDLAW A B, MORRISON A M. Induced side forces at high angles of attack[J]. Journal of Spacecraft & Rockets, 1976, 13(10):589-593.
[11] DENG X Y, WANG Y K. Asymmetric vortices flow over slender body and its active control at high angle of attack[J]. Acta Mechanica Sinica, 2004, 20(6):567-579.
[12] WILLIAMS D. A review of forebody vortex control scenarious:AIAA-1997-1967[R]. Reston:AIAA, 1997.
[13] ROOS F W, MAGNESS C L. Bluntness and blowing for flowfield asymmetry control on slender forebodies:AIAA-1993-3409[R]. Reston:AIAA, 1993.
[14] MALCOLM G N. Forebody vortex control-A progress review:AIAA-1993-3540[R]. Reston:AIAA, 1993.
[15] BERNHARDT J E, WILLIAMS D R. Proportional control of asymmetric forebody vortices[J]. AIAA Journal, 1998, 36(11):2087-2093.
[16] DENG X Y, BO N, CHEN Y, et al. The study of Reynolds number effect on the behaviors of asymmetric vortices flow[M]. Berlin:Springer Heidelberg, 2008:178-181.
[17] 邓学蓥, 詹慧玲, 王延奎. 单孔位微吹气扰动对非对称涡流动的主动控制[C]//第六届全国实验流体力学学术会议. 北京:中国力学学会, 2004. DENG X Y, ZHAN H L, WANG Y K. The active control of single-hole microblowing perturbation to asymmetric vortices flow[C]//Proceedings of the 6th Conference on Experimental Hydromechanics of China. Beijing:Chinese Society of Theoretical and Applied Mechanics, 2004(in Chinese).
[18] 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 Y S, MING X, Investigation on the characteristics and structures of unsteady flow filed near the zero-mass flux jet with PIV[J]. Journal of Experiments in Fluid Mechanics, 2005, 19(1):83-86(in Chinese).
[19] 明晓. 钝体尾流的特性及控制[D]. 南京:南京航空航天大学, 1988. MING X. The characteristics and control of blunt body wake[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 1988.
[20] 罗振兵, 夏智勋, 刘冰. 单膜双腔双口合成射流激励器:ZP200610031334.O[P]. 2006-08-16. LUO Z B, XIA Z X, LIU B. A synthetic jet actuator with a single diaphragm, dual cavities and exits:ZP200610031334.O[P]. 2006-08-16(in Chinese).
[21] LUO Z B, XIA Z X, LIU B. New generation of synthetic jet actuator[J]. AIAA Journal, 2006, 44(10):2418-2420.
[22] 邓雄, 夏智勋, 罗振兵, 等. 非对称出口合成双射流激励器矢量特性实验研究[J]. 航空学报, 2015, 36(2):510-517. DENG X, XIA Z X, LUO Z B, et al. Experimental investigation on the vectoring characteristic of dual synthetic jets actuator with asymmetric exits[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(2):510-517(in Chinese).
[23] 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 Z B, XIA Z X. Advances in synthetic jet technology and applications in flow control[J]. Advances in Mechanics, 2005, 35(2):221-234(in Chinese).1967,1997.
[15] Roos FW, Magness CL. Bluntness and blowing for flowfield asymmetry control on slender forebodies. AIAA Paper 93-3409, 1993.
[16] Malcolm GN. Forebody vortex control-A progreta review. AIAA 93-3540,1993.
[17] Williams D. A review of forebody vortex control scenarios. AIAA 97-1967, 1997.
[18] Bernhardt J E, Williams D R, Bernhardt J E. Proportional Control of Asymmetric Forebody Vortices[J]. Aiaa Journal, 2012, 36.
[19] Deng X Y, Bo N, Chen Y, et al. The Study of Reynolds Number Effect on the Behaviors of Asymmetric Vortices Flow[J]. New Trends in Fluid Mechanics Research, 2007:178-181.
[20] D.F. Fishe, D.G. Murri. Effect of Actuated Forebody Strakes on the Forebody Aerodynamics of the NASA F-18 HARV[J]. NASA Technical Memorandum 4774
[21] Deng Xueying, Zhan Huiling, Wang Yankui. The active control of single-hole micro-blowing perturbation to asymmetric vortices flow. The 6th Conference on Experimental Hydromechanics of China. 'Ihiyuan, Shanxi Province. 2004. (in Chinese)
邓学蓥, 詹慧玲, 王延奎. 单孔位微吹气扰动对非对称涡流动的主动控制[C]// 第六届全国实验流体力学学术会议. 2004.
[22] L Zhenbing, Xia Zhixun, Advances in synthetic jet technology and applications in flow control [J]. Advances in Mechanics, 2005, 35(2):221-234. DOI:doi:10.3321/j.issn:1000-0992.2005.02.009. (in Chinese)
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, 02期:221-234. DOI:doi:10.3321/j.issn:1000-0992.2005.02.009. |