SHOCK-BOUNDARY LAYER INTERACTION IN HYPERSONIC FLOW

被引：0
|
作者：
GAILLARD, L [1 ]
STORKMANN, V [1 ]
GRONIG, H [1 ]
机构：
[1] RHEIN WESTFAL TH AACHEN,STOSSWELLENLAB,D-52056 AACHEN,GERMANY
来源：
COMPTES RENDUS DE L ACADEMIE DES SCIENCES SERIE II FASCICULE B-MECANIQUE PHYSIQUE CHIMIE ASTRONOMIE | 1995年 / 321卷 / 05期
关键词：
D O I：
暂无
中图分类号：
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号：
07 ; 0710 ; 09 ;
摘要：
We study the hypersonic shock-flat plate boundary layer interaction. The boundary layer separation was detected. Its length is an increasing function of the Reynolds number at the interaction point (Re-X1). Downstream of the interaction, crossfluctuations of hat fluxes at the wall were observed; their amplitudes remain constant in terms of Re-X1; their average wavelength is invariant.
引用
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页码：183 / 186
页数：4
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