| [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.
|
| [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.
|
| [3] |
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.
|
| [4] |
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.
|
| [5] |
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.
|
| [6] |
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.
|
| [7] |
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.
|
| [8] |
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.
|
| [9] |
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.
|
| [10] |
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.
|
| [11] |
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.
|
| [12] |
Ma Guangyun;Shen Gongxin.
INVESTIGATION ON THE PROPERTIES AND STRUCTURES OF STARTING VORTEX FLOW AROUND 2-D BACKWARD-STEP BY PIV
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(3): 257-264.
|
| [13] |
Ji Zhou;Yin Xieyuan.
ANALYSIS OF UNSTEADY LEADING/SIDE-EDGE SEPARATED FLOW
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(6): 641-646.
|
| [14] |
Huang Shoulong;Wu Xiaosong;Xu Cheng.
NUMERICALSIMULATION OF VORTE4XFLOW IN AN OBLIQUE CAVITY USING TVD SCHEME
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(9): 1066-1069.
|
| [15] |
Li ke-wen;Lian Qi-xiang.
EXPERIMENTAL STUDY FOR THE HORSESHOE VORTEX IN TURBULENT BOUNDARY LAYER
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(2): 102-105.
|
CJA
