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

页码：T205 / T206

页数：2