REYNOLDS-NUMBER EFFECT ON SEPARATION STRUCTURES AT NORMAL SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTION

被引：8

作者：

DOERFFER, P ^{[1
]}

DALLMANN, U ^{[1
]}

机构：

[1] GERMAN AEROSP RES ESTAB,INST THEORET FLUID MECH,GOTTINGEN,FED REP GER

来源：

AIAA JOURNAL | 1989年 / 27卷 / 09期

关键词：

D O I：

10.2514/3.10247

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1206 / 1212

页数：7

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