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
收藏
页码：1206 / 1212
页数：7
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