TURBULENT BOUNDARY-LAYER WALL PRESSURE-FLUCTUATIONS DOWNSTREAM OF A TANDEM LEBU

被引：5

作者：

BEELER, GB

机构：

[1] NASA, Langley Research Cent,, Hampton, VA, USA, NASA, Langley Research Cent, Hampton, VA, USA

来源：

AIAA JOURNAL | 1986年 / 24卷 / 04期

关键词：

AERODYNAMICS; -; Turbulent;

D O I：

10.2514/3.9331

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Recent research has revealed that two rigid ribbons mounted in tandem and immersed in a turbulent boundary layer yield a net drag reduction 0 (10%). These ribbons are called large-eddy breakup devices (LEBUs). The LEBUs lower the downstream skin-friction coefficient up to 25%. The present experiment was performed to determine if the drag reduction is accompanied by a corresponding reduction in turbulent boundary-layer wall pressure fluctuations.

引用

页码：689 / 691

页数：3

共 8 条

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