Computational studies of the effect of wall temperature on hypersonic shock-induced boundary layer separation

被引：3
作者：
Brown, L. [1 ]
Fischer, C. [2 ]
Boyce, R. R. [1 ]
Reinartz, B. [2 ]
Olivier, H. [2 ]
机构：
[1] Univ New South Wales, Australian Def Force Acad, Northcott Dr, Canberra, ACT 2600, Australia
[2] Rhein Westfal TH Aachen, D-52064 Aachen, Germany
来源：
SHOCK WAVES, VOL 2, PROCEEDINGS | 2009年
关键词：
D O I：
10.1007/978-3-540-85181-3_70
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
引用
收藏
页码：1231 / +
页数：2
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PAGELLA A, 2004, M P RTO MP AVT 111 P
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REINARTZ B, 2006, 20068137 AIAA
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