Michael A, Florine C. Evolution of finite span synthetic jets [J]. Physics of Fluids, 2006, 18: 054101.
[2]
Yang A. Design analysis of a piezoelectrically driven synthetic jet actuator [J]. Smart Materials and Structures, 2009, 18(12): 125004.
[3]
Alvi F S, Cattafesta L N. The art and science of flow control - case studies using flow visualization methods [J]. The European Physical Journal Special Topics, 2010, 182(1): 97―112.
[4]
Sharma A S, Rawat V S, Kulkarni V, et al. Numerical investigations on flow control over blended-wing-body transonic aircraft using synthetic-jet actuators [J]. Journal of Aircraft, 2012, 49(2): 532―545.
[5]
明晓, 戴昌晖, 史胜熙. 声学整流效应的新现象[J]. 力学学报, 1992, 24(1): 48―54. Ming Xiao, Dai Changhui, Shi Shengxi. A new phenomenon of acoustic streaming [J]. Acta Mechanica Sinica, 1992, 24(1): 48―54. (in Chinese)
[6]
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 Yunsong, Ming Xiao. Investigation on the characteristics and structures of unsteady flow field near the Zero-mass flux jet with PIV [J]. Journal of Experiments in Fluid Mechanics, 2005, 19(1): 83―86. (in Chinese)
[7]
李念, 张堃元, 沙江, 等. 不同出口型与驱动频率的活塞型自耦合射流研究[J]. 航空动力学报, 2007, 22(3): 412―418. Li Nian, Zhang Kunyuan, Sha Jiang, et al. Experimental investigation of the characteristics of synthetic jet with different orifice aspect ratio and frequency [J]. Journal of Aerospace Power, 2007, 22(3): 412―418. (in Chinese)
[8]
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. (in Chinese)
[9]
Anderson W K, Thomas J L, Van Leer B. A comparison of finite volume flux vector splittings for the euler equations [J]. AIAA Journal, 1986, 24(9): 1453―1460.
[10]
Roe P L. Approximate riemann solvers, parameter vectors, and difference-schemes [J]. Journal of Computational Physics, 1981, 43(2): 357―372.
[11]
MacCormack R W, Candler G V. The solusion of the navier-stokes equations using gauss-seidel line relaxation [J]. Computers & Fluids, 1989, 17(1): 135―150.
[12]
Yoshiaki T, Kozo F. Conservation law for moving and transformed grids [C]. Orlando, 11th AIAA Computational Fluid Dynamics Conference, 1993: 733―742.
[13]
Eriksson L E. Generation of boundary conforming grids around wing-body configurations using transfinite interpolation [J]. AIAA Journal, 1982, 20(10): 1313―1320.
[14]
杨钧. 高超声速二维进气道性能研究[D]. 长沙: 国防科技大学, 2011: 29―30. Yang Jun. Performance research of 2-D hypersonic inlet [D]. Changsha: National University of Defense Technology, 2011: 29―30. (in Chinese)
[15]
Smith B L, Swift G W. A comparison between synthetic jets and continuous jets [J]. Experiments in Fluids, 2003, 34(4): 467―472.
[16]
罗振兵, 夏智勋. 合成射流技术及其在流动控制中的应用进展[J]. 力学进展, 2005, 35(2): 221―234. Luo Zhenbing, Xia Zhixun. Advances in synthetic jet technology and applications in flow control [J]. Advances In Mechanics, 2005, 35(2): 221―234. (in Chinese)
[17]
Seifert A, Bachar T, Koss D, et al. Oscillatory blowing: A tool to delay boundary-layer separation [J]. AIAA Journal, 1993, 31(11): 2052―2060.
[18]
Wiltse J, Glezer A. Manipulation of free shear flows using piezoelectric actuators [J]. Journal of Fluid Mechanics, 1993, 249: 261―285.
