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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2016, Vol. 37 ›› Issue (4): 1083-1091.doi: 10.7527/S1000-6893.2015.0263

• Fluid Mechanics and Flight Mechanics •     Next Articles

Wall temperature effect on hypersonic vehicle drag

LIU Jie1,2, WANG Jikang2, LONG Shuangli2, GUAN Chengqi2, XIANG Jinwu1   

  1. 1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China;
    2. Beijing Aerospace Technology Institute, Beijing 100074, China
  • Received:2015-06-08 Revised:2015-09-25 Online:2016-04-15 Published:2015-10-19
  • Supported by:

    National Natural Science Foundation of China (91216102)

Key words: hypersonic, wall temperature, aerodynamic drag, numerical simulation, wind tunnel test

CLC Number: