[1] |
JIA Yunze, SANG Weimin, CAI Yang.
Anti-icing property of NSDBD plasma actuator based on numerical simulation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(4): 121652-121652.
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[2] |
ZHANG Xin, HUANG Yong, YANG Pengyu, ZHANG Peng, HUANG Zhiyuan, WANG Dawei, LI Huaxing.
Flight test of flow separation control using plasma UAV
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 121587-121587.
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[3] |
HONG Shuli, HUANG Guoping.
Introducing DMD method to study dynamic structures of flow separation with and without control
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(8): 120876-120876.
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[4] |
LIANG Hua, WU Yun, LI Jun, HAN Menghu, MA Jie.
Test of high lift system flow control by plasma aerodynamic actuation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(8): 2603-2613.
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[5] |
KANG Wei, ZHANG Quanqi, DAI Xiangyan, LIU Lei.
A method for effectiveness analysis of flow separation control by local actuation based on Lagrangian coherent structures
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(8): 2490-2497.
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[6] |
DU Hai, SHI Zhiwei, CHENG Keming, LI Ganniu, SONG Tianwei, LI Zheng.
Frequency optimization and vortex dynamic process analysis of separated flow control by nanosecond pulsed plasma discharge
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(7): 2102-2111.
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[7] |
LI Binbin, YAO Yong, GU Yunsong, CHENG Keming.
Active control of 2D backward facing step separated flow based on synthetic jet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(6): 1753-1762.
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[8] |
LI Yujie, LUO Zhenbing, DENG Xiong, SUN Jian, SHEN Zheng.
Experimental investigation on flow separation control of stalled NACA0015 airfoil using dual synthetic jet actuator
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(3): 817-825.
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[9] |
ZHAO Guangyin, LIANG Hua, LI Yinghong, HAN Menghu, HUA Weizhuo.
Experiment of flow control on a low swept delta wing using pulsed nanosecond plasma actuation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(7): 2125-2132.
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[10] |
WU Yun, LI Yinghong.
Progress and outlook of plasma flow control
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(2): 381-405.
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[11] |
KANG Wei, LIU Lei, XU Min, LEI Pengfei, ZHANG Jiazhong.
Lift enhancement mechanism for local oscillation of airfoil surface at low Reynolds number
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(11): 3557-3566.
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[12] |
GAO Wenzhi, LI Zhufei, YANG Jiming.
Flow characteristics experiments of a hypersonic axisymmetric inlet with nose bluntness
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 302-310.
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[13] |
YU Ping, DUAN Yi, CHEN Jun.
Some aerodynamic issues in hypersonic flight
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 7-23.
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[14] |
YANG Pengyu, ZHANG Bailing, LI Yiwen, ZHANG Yang.
Experimental Study of the Discharge Characteristic of Nanosecond Voltage Pulses in Supersonic Flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(6): 1539-1548.
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[15] |
ZHANG Haideng, LI Yinghong, WU Yun, ZHAO Qin.
Simulation Research of Nanosecond Pulsed Plasma Actuation Flow Control on High Speed Compressor Cascade
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(6): 1560-1570.
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