SUPERSONIC SEPARATED AND REATTACHING LAMINAR FLOWS .1. GENERAL THEORY AND APPLICATION TO ADIABATIC BOUNDARY-LAYER-SHOCK-WAVE INTERACTIONS

被引：129

作者：

LEES, L

REEVES, BL

机构：

来源：

关键词：

D O I：

10.2514/3.2700

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1907 / 1920

页数：14

共 41 条

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CROCCO, L
LEES, L
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