[1] |
Yifeng HUANG, Shuhua ZENG, Zhongzheng JIANG, Weifang CHEN.
Numerical study on high-altitude lateral jet based on nonlinear coupled constitutive relation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 8-22.
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[2] |
LIU Pengxin, YUAN Xianxu, SUN Dong, FU Yalu, LI Chen.
Direct numerical simulation of high-temperature turbulent boundary layer with chemical nonequilibrium
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 124877-124877.
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[3] |
REN Weijie, XIE Wenjia, TIAN Zhengyu, ZHANG Ye, YU Hang.
Grid dependence of hypersonic numerical shock instability
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726376-726376.
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[4] |
XIANG Xinghao, ZHANG Yifeng, YUAN Xianxu, TU Guohua, WAN Bingbing, CHEN Jianqiang.
C-γ-Reθ model for hypersonic three-dimensional boundary layer transition prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 625711-625711.
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[5] |
WU Han, WANG Jianhong, HUANG Wei, DU Zhaobo, YAN Li.
Research progress on shock wave/boundary layer interactions and flow controls induced by micro vortex generators
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 25371-025371.
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[6] |
LI Jin, GENG Xiangren, CHEN Jianqiang, JIANG Dingwu, LI Hongzhe.
Numerical simulation on DSMC quantum kinetic chemical reaction model
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 122176-122176.
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[7] |
PENG Jun, ZHANG Zijian, ZHOU Kai, HU Zongmin, JIANG Zonglin.
Effects of vibration excitation on shock reflections
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(8): 121055-121055.
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[8] |
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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[9] |
YAN Zhenguo, LIU Huayong, MAO Meiliang, MA Yankai, ZHU Huajun.
Development of 3rd-order HWCNS and its application in hypersonic flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(5): 1460-1470.
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[10] |
LI Haiyan, TANG Zhigong, YANG Yanguang, SHI Anhua, LUO Wanqing.
Problems of numerical simulation of high-temperature gas flow fields for hypersonic vehicles
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 176-191.
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[11] |
WU Ziniu, BAI Chenyuan, LI Juan, CHEN Zijun, JI Shixiang, WANG Dan, WANG Wenbin, XU Yizhe, YAO Yao.
Analysis of flow characteristics for hypersonic vehicle
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 58-85.
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[12] |
TANG Zhigong, ZHANG Yirong, CHEN Jianqiang, MAO Meiliang, ZHANG Yifeng, LIU Huayong.
More fidelity, more accurate, more efficient—progress on numerical simulations for hypersonic flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 120-134.
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[13] |
GAO Wenzhi, LI Zhufei, YANG Jiming.
Flow characteristics experiments of a hypersonic axisymmetric inlet with nose bluntness
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 302-310.
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[14] |
ZHANG He, ZHONG Chengwen, GONG Jian, BI Zhixian, HAN Shuguang.
Adaptive Mesh Refinement for Gas-kinetic BGK Scheme
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(3): 687-694.
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[15] |
KONG Weixuan, YAN Chao, ZHAO Rui.
Effect of Wall Temperature on Boundary Layer Transition Prediction Using Transition Model
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(10): 2249-2255.
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