TURBULENT-BOUNDARY-LAYER DEVELOPMENT IN AN ADVERSE PRESSURE GRADIENT AFTER AN INTERACTION WITH A NORMAL SHOCK WAVE.

被引：0

作者：

Schofield, W.H. ^{[1
]}

机构：

[1] Aeronautical Research Lab, Melbourne, Aust, Aeronautical Research Lab, Melbourne, Aust

来源：

Journal of Fluid Mechanics | 1985年 / 154卷

关键词：

ADVERSE PRESSURE GRADIENT - TURBULENT-BOUNDARY-LAYER;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：43 / 62

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[1] TURBULENT-BOUNDARY-LAYER DEVELOPMENT IN AN ADVERSE PRESSURE-GRADIENT AFTER AN INTERACTION WITH A NORMAL SHOCK-WAVE
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