| [1] |
Jiang LAI, Zhaolin FAN, Qian WANG, Siwei DONG, Fulin TONG, Xianxu YUAN.
Direct numerical simulation of hypersonic cone-flare model at angle of attack
[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128610-128610.
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| [2] |
Rubing LIU, Zefan CHEN, Ruixin LIN, Qi LIN.
Active control of flow-induced vibration of blades in a plane cascade by a plasma synthetic jet
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 128430-128430.
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| [3] |
Canmin LI, Hexia HUANG, Gang LIANG, Jinghao LYU, Jia CAI, Huijun TAN.
Flow control method for impinging shock/boundary-layer interaction based on swept-back cowl configuration
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(16): 128091-128091.
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| [4] |
Jiangsheng WANG, Jinjun WANG.
Vortex/boundary⁃layer interactions over multi⁃element airfoil at low Reynolds number
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(12): 127652-127652.
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| [5] |
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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| [6] |
Hai DU, Lejie YANG, Zheng LI, Yue XU, Jingyang SUN, Yuhang WANG.
Lifting mechanism and energy efficiency analysis of multistage circulation control technology
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 54-66.
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| [7] |
QIN Chen, ZHANG Rongping, ZHANG Junlong, YUE Tingrui, WU Songling.
Acoustic performance of an under-expanded supersonic jet with different impinging distances to an inclined plate
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 125857-125857.
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| [8] |
TONG Fulin, DONG Siwei, DUAN Junyi, LI Xinliang.
Direct numerical simulation of separation bubble in shock wave/turbulent boundary layer interaction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 125437-125437.
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| [9] |
TONG Fulin, ZHOU Guiyu, SUN Dong, LI Xinliang.
Expansion effect on shock wave and turbulent boundary layer interactions
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 123731-123731.
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| [10] |
ZHANG Yongjie, WU Yingying, ZHAO Shuwang, SI Jiangtao, YUAN Changsheng.
Review of non-circular cross-section fuselage structure design research on blended-wing-body civil aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(9): 623054-623054.
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| [11] |
XUE Shuaijie, LIU Hongjun, CHEN Pengfei, XIA Yizhi.
Test on spray stability of swirl injector with gas injection
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(7): 122697-122697.
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| [12] |
LI Jian, ZHANG Hua, WU Xinggang.
Junction flow horseshoe vortex control based on upstream cavity
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(6): 120796-120796.
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| [13] |
ZHU Rui, LIU Jinsheng, LIU Zhirong, BAO Feng.
Experiment on a new concept wing layout with alleviated wake vortex
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(4): 120250-120250.
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| [14] |
LIU Qiang, LIU Qiang, BAI Peng, LI Feng.
Aerodynamic characteristics of airfoil and evolution of laminar separation at different Reynolds numbers
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(4): 120338-120338.
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| [15] |
WANG Kelei, ZHU Xiaoping, ZHOU Zhou, WANG Hongbo.
Distributed electric propulsion slipstream aerodynamic effects at low Reynolds number
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(9): 2669-2678.
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