[1] |
Heng ZHANG, Jie LI, Binbin ZHAO.
Improvement mechanism of ice-tolerance capacity for iced airfoil with variable camber of drooping leading edge
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627114-627114.
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[2] |
SUN Dong, LIU Pengxin, SHEN Pengfei, TONG Fulin, GUO Qilong.
Direct numerical simulation of shock wave/turbulent boundary layer interaction in hollow cylinder-flare configuration at Mach number 6
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 124681-124681.
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[3] |
XIE Lu, ZHANG Yanjun, HOU Yinzhu, LIU Wei, LEI Wutao.
Cavity flow pressure characteristics and flow control methods of subsonic weapon bay
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 123961-123961.
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[4] |
LIU Jun, CAI Jinsheng, YANG Dangguo, SHI Ao, LU Bo.
Research progress in wave evolution and noise control for supersonic cavity flows
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(11): 22366-022366.
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[5] |
SHI Xiaojun, LI Yonghong, LIU Dawei, CHANG Lixia, YANG Ke.
Asymmetric flow mechanism for small aspect ratio rudders with large deflection angles on rotated missile
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(9): 2690-2698.
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[6] |
DONG Xiangrui, CHEN Yaohui, DONG Gang, LIU Yixin.
DES numerical study of shock wave/boundary layer interactions in hypersonic flows controlled by double micro-ramps
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(6): 1771-1780.
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[7] |
YANG Zhanyu, SHAN Peng, ZHAO Lushun, JIE Ke, GUO Desan, LIU Jian, HUANG Yong.
Experimental Study on Flame Holding Torch of a Hydrocarbon Fueled Combined Supersonic Combustor with a Pilot Burner and a Streamwise-vortices Generator
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, (3): 390-401.
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[8] |
GU Yun-song;MING Xiao.
Proportional Side Force Control of Slender Body at High Angle of Attack
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(5): 746-750.
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[9] |
LIU Pei-qing;SHAO Yan-feng;DENG Xue-ying;MA Yu.
Experimental Study of the Evolutionary Process of the Flowfield Around Slender Body at High Angle of Attack
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2003, 24(6): 503-506.
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[10] |
GU Yun-song;MING Xiao.
Forebody Vortices Control Using a Fast-Swinging Micro-Tip-Strake at High Angles of Attack
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2003, 24(2): 102-106.
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[11] |
Huang Hongyan;Han Wanjing;Wang Zhongqi.
FLOW OBSERVATION OF TOPOLOGICAL AND VORTICAL STRUCTURE IN TURBINE ROTOR CASCADES WITH TIP CLEARANCE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(3): 257-261.
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[12] |
Shen Mengyu;Liu Qiusheng;Guo Yanhu;Wang Baoguo.
COMPUTATIONS AND VORTEX ANALYSIS OF THREE DIMENSIONAL TURBULENT FLOW FIELDS IN A TRANSONIC COMPRESSOR ROTOR
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(6): 82-85.
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[13] |
Yan Chao;Chen Liang.
NUMERICAL SIMULATION OF THREE DIMENSIONAL SEPARATED AND VORTICAL FLOW OVER HEMISPHERE CYLINDER
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(6): 91-94.
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[14] |
Hong Jinsen.
TYPES OF FLOW OVER LEESIDE OF A CLIPPED DELTA WING AT SUPERSONIC SPEEDS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(5): 90-95.
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[15] |
Le Guigao;Ma Dawei;Zhang Fuxiang.
NUMERICAL AND EXPERIMENTAL STUDIES OF JET FLOW EXHAUSTING FROM ROCKET
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(5): 75-78.
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