[1] |
Haixing LI, Feng ZHOU, Wei YAN, Feng BAI, Keliang ZHAO.
Effects of roughness ice on aerodynamic performance of civil aircraft horizontal tail
[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128657-128657.
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[2] |
Xueliang LI, Chuangchuang LI, Wei SU, Jie WU.
Experiment of influence of distributed roughness elements on hypersonic boundary layer instability
[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128627-128627.
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[3] |
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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[4] |
Fanyu ZENG, Yunlong QIU, Zhanwei CAO, Lun ZHANG, Weifang CHEN.
Flow control and drag reduction characteristics of micro-blowing array on supersonic turbulent boundary layer
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729396-729396.
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[5] |
Junlin LIU, Xihai XU, Zhicheng ZHANG, Xiaoqian CHEN.
Simulation and analysis of noise reduction in high⁃temperature and high⁃speed rocket jet by water injection
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 127122-127122.
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[6] |
Weijia LIU, Yingkun LI, Xiong CHEN, Chunlei LI.
Panel flutter characteristics on shock wave/boundary layer interaction based on fluid⁃structure coupling
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127085-127085.
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[7] |
Hongkang LIU, Jianqiang CHEN, Xinghao XIANG, Yatian ZHAO.
Transition prediction for HIAD with different Reynolds numbers by improved k-ω-γtransition model
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 126868-126868.
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[8] |
Zongyao YANG, Jingzhou ZHANG, Yong SHAN.
Suppression of exhaust plume infrared and jet noise of large aspect ratio curved mixing duct
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 126848-126848.
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[9] |
Jiahui SONG, Aiguo XU, Long MIAO, Yugan LIAO, Fuwen LIANG, Feng TIAN, Mingqing NIE, Ningfei WANG.
Entropy increase characteristics of shock wave/plate laminar boundary layer interaction
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 528520-528520.
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[10] |
Mengge WANG, Xiaoming HE, Juanjuan WANG, Yue ZHANG, Kun WANG, Huijun TAN, Liugang LI.
Shock wave/boundary layer interaction control method based on oscillating vortex generator
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 128503-128503.
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[11] |
Fangcheng SHI, Zhenxun GAO, Yuyan TIAN, Chongwen JIANG, Tiantian WANG, Chun-Hian LEE.
Large eddy simulation of ideally expanded supersonic jet noise
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626266-626266.
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[12] |
Di WANG, Yan LENG, Long YANG, Zhonghua HAN, Zhansen QIAN.
Atmospheric turbulence effects on sonic boom propagation based on augmented Burgers equation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626318-626318.
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[13] |
Shanshan TIAN, Liang JIN, Zhaobo DU, Xiangyu ZHONG, Wei HUANG, Yuanyang LIU.
Research progress of shock wave/boundary layer interaction controls induced by bump
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(18): 28411-028411.
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[14] |
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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[15] |
Guangsheng ZHU, Shiyong YAO, Yi DUAN.
Research progress and engineering application of flow control technology for drag and heat reduction of high-speed vehicles
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 529049-529049.
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