[1] |
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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[2] |
Ping MA, Ning ZHANG, Anhua SHI, Zhefeng YU, Shichang LIANG, Jie HUANG.
Transmission characteristics of typical band microwave in experiment⁃simulated plasma
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729476-729476.
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[3] |
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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[4] |
LIU Qiang, TU Guohua, LUO Zhenbing, CHEN Jianqiang, ZHAO Rui, YUAN Xianxu.
Progress in hypersonic boundary layer transition delay control
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 25357-025357.
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[5] |
LI Qiang, WAN Bingbing, YANG Kai, ZHU Tao.
Experimental research on characteristics of pressure and heat flux fluctuation in hypersonic cone boundary layer
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 124956-124956.
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[6] |
YANG Peng, TANG Zhigong, CHEN Jianqiang, YUAN Xianxu, CHEN Xi, DONG Siwei.
Temporal evolution of wavepackets on the windward side of an inclined hypersonic cone under a flight condition
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726367-726367.
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[7] |
CHEN Suyu, JIANG Tao, CHANG Yu, HU Shouchao, LI Qiang, ZHANG Kouli.
Hypersonic boundary layer transition over bodies with blunt nosetip
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 124098-124098.
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[8] |
ZHANG Yanjun, DUAN Zhuoyi, LEI Wutao, BAI Junqiang, XU Jiakuan.
Design of supercritical natural laminar flow wing and its boundary layer transition wind tunnel test based on TSP technique
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 122429-122429.
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[9] |
SONG Wei, ZHAO Xiaojian, LU Wei, JIANG Zenghui.
Effect of boundary layer transition on free flight motion of hypersonic spinning blunt cone
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(11): 121295-121295.
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[10] |
GUO Yijun, ZHOU Yu, XIAO Hanshan, ZHOU Shuguang, QIU Bo, ZENG Lei, LIU Xiao.
Delay phenomenon of boundary layer transition according to heating flux identified from flight test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(10): 121255-121255.
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[11] |
ZHAN Dongwen, YANG Jianting, YANG Jiming, ZHU Yujian.
A new method of wall profile design for shape-controllable shock wave enhancement
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(8): 2408-2416.
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[12] |
DUAN Zhiwei, XIAO Zhixiang.
Roughness element induced hypersonic boundary layer transition
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(8): 2454-2463.
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[13] |
ZHOU Ling, YAN Chao, HAO Zihui, KONG Weixuan, ZHOU Yu.
Transition model and transition criteria for hypersonic boundary layer flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(4): 1092-1102.
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[14] |
XU Jiakuan, BAI Junqiang.
Amplification factor transport model based on boundary layer similarity solution
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(4): 1103-1113.
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[15] |
TU Guohua, YAN Zhenguo, ZHAO Xiaohui, MA Yankai, MAO Meiliang.
SA and SST turbulence models for hypersonic forced boundary layer transition
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(5): 1471-1479.
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