Wall temperature effect on hypersonic vehicle drag

LIU Jie; WANG Jikang; LONG Shuangli; GUAN Chengqi; XIANG Jinwu

doi:10.7527/S1000-6893.2015.0263

ACTA AERONAUTICAET ASTRONAUTICA SINICA >

2016 , Vol. 37 >Issue 4: 1083 - 1091

DOI: https://doi.org/10.7527/S1000-6893.2015.0263

Fluid Mechanics and Flight Mechanics

Wall temperature effect on hypersonic vehicle drag

LIU Jie ,
WANG Jikang ,
LONG Shuangli ,
GUAN Chengqi ,
XIANG Jinwu

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1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China;
2. Beijing Aerospace Technology Institute, Beijing 100074, China

Received date: 2015-06-08

Revised date: 2015-09-25

Online published: 2015-10-19

Supported by

National Natural Science Foundation of China (91216102)

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Abstract

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

Cite this article

LIU Jie , WANG Jikang , LONG Shuangli , GUAN Chengqi , XIANG Jinwu . Wall temperature effect on hypersonic vehicle drag[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016 , 37(4) : 1083 -1091 . DOI: 10.7527/S1000-6893.2015.0263

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