SCALING OF STEP-INDUCED SUBSONIC TURBULENT BOUNDARY-LAYER SEPARATION

被引：0
|
作者：
ELFSTROM, GM
机构：
来源：
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK | 1986年 / 66卷 / 04期
关键词：
FRICTION - PRESSURE MEASUREMENT;
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
An experimental investigation of the subsonic separated turbulent boundary layer over a forward-facing step has revealed that there are two distinct regions of the flow. One, the farfield, is seen to scale on step-height alone, once the Prandtl-Glauert rule is applied. The notion of the boundary layer behaving as an inviscid rotational stream has been used to explain trends in the nearfield.
引用
收藏
页码：T205 / T206
页数：2
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