[1] WRIGHT M C M, NELSON P A. Wind tunnel experiments on the optimization of distributed suction for laminar flow control[J]. Proceedings of the Institution of Mechanical Engineers, 2001, 215(6):343.
[2] ZAMAN K B. Effect of acoustic exciation on the flow over a low-Re airfoil[J]. Journal of Fluid Mechanics, 1987, 182(4):127-148.
[3] ARGA S P S. Buoyancy effects in a horizontal flat-plate boundary layer[J]. Journal of Fluid Mechanics, 1975, 68(2):321-343.
[4] MALIK M R.Ion wind drag reduction[C]//21st Aerospace Sciences Meeting. Reston:AIAA, 1983:203-208.
[5] ROTH J R.Interaction of electromagentic fields with magnetized plasmas[R]. Tennessee:Tennessee University, 1994.
[6] ROTH J R.Investigation of a uniform glow discharge plasma in atmospheric air[R]. Tennessee:Tennessee University, 1994.
[7] ROTH J R,Sherman D M.Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma[C]//36th AIAA Aerospace Science Meeting including the New Horizons Forum and Aerospace Exposition. Reston:AIAA, 1997:113-119.
[8] GRUNDMANN S, CAMERON T. Experimental transition delay using glow-discharge plasma actuators[J]. Experiments in Fluids, 2007, 42(4):653-657.
[9] GRUNDMANN S, TROPEA C. Active cancellation of artificially introduced Tollmien-Schlichting waves using plasma actuators[J]. Experiments in Fluids, 2008, 44(5):795-806.
[10] DUCHMANN A, SIMON B, MAGIN P, et al. In-flight transition delay with DBD plasma actuators[C]//51st AIAA Aerospace Science Meeting including the New Horizons Forum and Aerospace Exposition. Reston:AIAA, 2013:103-114.
[11] HANSON R E, LAVOIE P, BADE K M,et al.Steady-state closed-loop control of bypass boundary layer transition using plasma actuators[C]//50st AIAA Aerospace Science Meeting including the New Horizons Forum and Aerospace Exposition. Reston:AIAA, 2012:82-95.
[12] BELSON B A, MEIDELL K, HANSON R,et al.Comparison of plasma actuators in simulations and experiments for control of bypass transition[C]//50th AIAA Aerospace Science Meeting including the New Horizons Forum and Aerospace Exposition. Reston:AIAA, 2012:101-109.
[13] 史志伟, 范本根. 不同结构等离子体激励器流场特性实验研究[J]. 航空学报, 2011, 32(9):1583-1589. SHI Z W, FAN B G. Experimental study on flow field characteristics of different plasma actuators[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(9):1583-1589(in Chinese).
[14] 杜海, 史志伟. 等离子体激励器对微型飞行器横航向气动力矩控制的实验研究[J]. 航空学报, 2012, 32(10):1781-1790. DU H, SHI Z W. Experimental study of directional-lateral aerodynamic moment control of micro air vehicle by plasma actuators[J]. Acta Aeronautica et Astronautica Sinca, 2012, 32(10):1781-1790(in Chinese).
[15] 杜海. 等离子体流动控制技术及其在飞行器上的应用研究[D]. 南京:南京航空航天大学, 2012. DU H. Plasma flow control technology and its application on flight vehicle[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012(in Chinese). |