| Citation: | HUA Wei-zhuo, LI Ying-hong, NIU Zhong-guo, ZHAO Guang-yin, LIANG Hua, HAN Meng-hu. Experiment on low-speed delta wing using nanosecond pulse plasma actuation[J]. Journal of Aerospace Power, 2014, (10): 2331-2339. doi: 10.13224/j.cnki.jasp.2014.10.008 |
| [1] |
Roupassov D V,Nikipelov A A,Nudnova M M,et al.Flow separation control by plasma actuator with nanosecond pulse periodic discharge[R].AIAA-2008-1367,2008.
|
| [2] |
李应红,梁华,马清源,等.脉冲等离子体气动激励抑制翼型吸力面流动分离的实验研究[J].航空学报,2008,29(6):1429-1435. LI Yinghong,LIANG Hua,MA Qingyuan,et al.Experimental investigation on airfoil suction side flow separation by pulse plasma aerodynamic actuation[J].Acta Aeronautica et Astronautica Sinica,2008,29(6):1429-1435.(in Chinese)
|
| [3] |
赵小虎,吴云,李应红,等.高负荷压气机叶栅分离结构及其等离子体流动控制[J].航空学报,2012,33(2):208-219. ZHAO Xiaohu,WU Yun,LI Yinghong,et al.Separation structure and plasma flow control on highly loaded compressor cascade[J].Acta Aeronautica et Astronautica Sinica,2012,33(2):208-219.(in Chinese)
|
| [4] |
Nishihara M,Takashima K,Rich J,et al.Mach 5 bow shock control by a nanosecond pulse surface DBD[R].AIAA-2011-1144,2011.
|
| [5] |
Kwak D Y,Nelson R C.Vortical flow control over delta wings with different sweep back angles using DBD plasma actuators[R].AIAA-2010-4837,2010.
|
| [6] |
秦燕华,庄逢甘,沈礼敏,等.展向射流控制机翼前缘涡的机理及其应用[J].空气动力学学报,1998,16(3):267-275. QIN Yanhua,ZHUANG Fenggan,SHEN Limin,et al.An experimental study on controlling vortex over wing by using spanwise blowing[J].Acta Aerodynamica Sinica,1998,16(3):267-275.(in Chinese)
|
| [7] |
Visbal M R,Gaitonde D V.Control of vortical flows using simulated plasma actuators[R].AIAA-2006-505,2006.
|
| [8] |
Zhang P F,Wang J J,Feng L H,et al.Experimental study of plasma flow control on highly swept delta wing[J].AIAA Journal,2010,48(1):249-252.
|
| [9] |
Greenblatt D,Kastantin Y,Nayeri C N,et al.Delta-wing flow control using dielectric barrier discharge actuators[R].AIAA-2007-4277,2007.
|
| [10] |
梁华,李应红,贾敏,等.等离子体气动激励的能量转化过程分析[J].高电压技术,2010,36(12):3054-3058. LIANG Hua,LI Yinghong,JIA Min,et al.Energy conversion process analysis of plasma aerodynamic actuation[J].High Voltage Engineering,2010,36(12):3054-3058.(in Chinese)
|
| [11] |
Glaz B,Dinavahi S P G,Gaitonde D V.Nanosecond pulsed plasma actuation effects on aerodynamic damping and implications for aeroelastic stability in the post-stall regime[R].AIAA-2012-1482,2012.
|
| [12] |
李应红,吴云,梁华,等.提高抑制流动分离能力的等离子体冲击流动控制原理[J].科学通报,2010,55(31):3060-3068. LI Yinghong,WU Yun,LIANG Hua,et al.The mechanism of plasma shock flow control for enhancing flow separation control capability[J].Chinese Science Bulletin,2010,55(31):3060-3068.(in Chinese)
|
| [13] |
Gursul I,Wang Z,Vardaki E.Review of flow control mechanisms of leading-edge vortices[J].Progress in Aerospace Sciences,2007,43(7):246-270.
|
| [14] |
Lowson M V,Riley A J.Vortex breakdown control by delta wing geometry[J].Journal of Aircraft,1995,32(4):832-838.
|
| [15] |
李凤蔚.空气与气体动力学引论[M].西安:西北工业大学出版社,2007:495-505.
|
| [16] |
Polhamus E C.Prediction of vortex lift characteristics by a leading-edge suction analogy[J].Journal of Aircraft,1971,8(4):193-199.
|
| [17] |
WANG Jinjun,XU Yan.Experimental studies on control of delta wing aerodynamics[R].AIAA-2004-252,2004.
|
| [18] |
顾祥玉,杨永,李喜乐.马赫数和雷诺数对钝前缘三角翼流场的影响[J].航空计算技术,2012,42(6):13-16. GU Xiangyu,YANG Yong,LI Xile.Numerical simulation for effects of Mach and Reynolds number on flow over medium radius leading edge delta wing[J].Aeronautical Computing Technique,2012,42(6):13-16.(in Chinese)
|