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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A Detonation Tunnel with High Temperature Burnt Gas as Test Medium
LI Jin-ping, ZHANG Shi-zhong, YU Jiang-peng, ZHANG Xiao-yuan, CHEN Hong, YU Hong-ru
2018, 3(6): 1-8. DOI: 10.19527/j.cnki.2096-1642.2018.06.001
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A Combined Theoretical and Experimental Study on the Reaction Kinetics of Ethyl Formate with the Hydroxyl Radical
WU Jun-jun, Fethi Khaled, Aamir Farooq, REN Wei
2018, 3(6): 9-15. DOI: 10.19527/j.cnki.2096-1642.2018.06.002
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Experimental on Air-Breathing Rotating Detonation Engine Using Ethylene or Hydrogen
WANG Yu-hui, WANG Chao, ZHENG Yu-shan, LE Jia-ling, HUANG Si-yuan
2018, 3(6): 16-25. DOI: 10.19527/j.cnki.2096-1642.2018.06.003
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Experimental Investigation on Aero-optics Imitation of Hypersonic Optical Dome with Supersonic Film
DING Hao-lin, YI Shi-he, ZHAO Xin-hai, YI Jun-ru, GE Yong
2018, 3(6): 26-34. DOI: 10.19527/j.cnki.2096-1642.2018.06.004
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Investigation and Optimization of Acoustic Metasurfaces to Depress Mack Second Mode in Hypersonic Boundary-Layer Flow
ZHAO Rui, ZHANG Xin-xin, WEN Chihyung, TIAN Xu-dong
2018, 3(6): 35-40. DOI: 10.19527/j.cnki.2096-1642.2018.06.005
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Numerical Simulation of Supersonic Flow/Jet Interaction at the Double Backward-Facing Step
DENG Fang, HAN Gui-lai, MENG Bao-qing, DING Jue, WENG Pei-fen, HAN Peng, JIANG Zong-lin
2018, 3(6): 41-50. DOI: 10.19527/j.cnki.2096-1642.2018.06.006
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Effects of Vortex Generators on the External Flows of an Axisymmetric Hypersonic Inlet
GAO Wen-zhi, CAO Rao, LI Zhu-fei, ZENG Yi-shan, YANG Ji-ming
2018, 3(6): 51-62. DOI: 10.19527/j.cnki.2096-1642.2018.06.007
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