Axisymmetric separated shock-wave boundary-layer interaction

被引：0

作者：

Murray, N. ^{[1
]}

Hillier, R. ^{[1
]}

机构：

[1] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England

来源：

SHOCK WAVES, VOL 2, PROCEEDINGS | 2009年

关键词：

HEAT-TRANSFER;

D O I：

10.1007/978-3-540-85181-3_69

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：1225 / 1230

页数：6

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