Supervised by： China Aerospace Science and Technology Corporation
Sponsored by： China Academy of Aerospace Aerodynamics
Chinese Society of Astronautics
China Aerospace Publishing House Co., LTD

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Cover and contents of Vol.8 No.3
2023, 8(3)
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Review on Oblique Transition
DENG Ze-feng, CHEN Xi, ZHANG Chuan-hong
2023, 8(3): 1-18. DOI: 10.19527/j.cnki.2096-1642.1018
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Progress on Prediction Models for Crossflow Instabilities Dominated Transition Based on Local Variables
XU Jia-kuan, DUAN Yi, YANG Jia-sheng, QIAO Lei, LIU Jian-xin, BAI Jun-qiang
2023, 8(3): 19-34. DOI: 10.19527/j.cnki.2096-1642.1012
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Evolution of Supersonic Modes in Hypersonic High-Enthalpy Boundary Layer Transition
ZHAO Zhou-yuan, CHEN Xian-liang, WANG Liang, FU Song
2023, 8(3): 35-45. DOI: 10.19527/j.cnki.2096-1642.1023
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Numerical Simulation of Heat Reduction With Use of Spike in Hypersonic Flow Based on Gas Kinetic Scheme
LIU Chang-ya, ZHOU Di, LU Zhi-liang, GUO Tong-qing
2023, 8(3): 46-54. DOI: 10.19527/j.cnki.2096-1642.1016
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Aeroheating of the Main Engine Jet of a Reusable Launch Vehicle
LI Xiao-yan, CAI Qiao-yan, SHI Wei, LIU Jie-ping, ZHAO Ling, LYU Jun-ming
2023, 8(3): 55-63. DOI: 10.19527/j.cnki.2096-1642.1001
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Engineering Estimation Method of Large Expansion Ratio Nozzle Performance
HUANG Rong, JIA Yao-qiang, LI Bin
2023, 8(3): 64-69. DOI: 10.19527/j.cnki.2096-1642.1009
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Influence of the Turbopump Exhaust on the Aerodynamic Performance of Supersonic Aircraft
JIANG Xi-hang, MA Lin-jing
2023, 8(3): 70-76. DOI: 10.19527/j.cnki.2096-1642.0996
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Application of a Two-Step Chemical Scheme for Kerosene in Supersonic Combustion with Low Total Temperature
LI Ji, REN Hu, TIAN Ye, LIU Yuan, YANG Shun-hua
2023, 8(3): 77-86. DOI: 10.19527/j.cnki.2096-1642.0994
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