Experiments on Mach-wave interactions in a compressible shear layer

被引:11
作者
Doty, MJ [1 ]
McLaughlin, DK [1 ]
机构
[1] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
关键词
D O I
10.2514/2.840
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A potential technique for improving the growth rate of compressible shear layers is studied, in which a wavy-wall geometry is configured in a confined supersonic shear-layer facility that generates Mach waves in the flowfield, The major objective of this work is to evaluate a numerical model that predicts the growth properties of a three-way resonant interaction of these spatial Mach waves with duct acoustic waves and Kelvin-Helmholtz waves excited artificially or naturally within the shear layer. Measurements show that a tuned pore tone excitation of Kelvin-Helmholtz waves couples with the wavy-wall-induced disturbances and duct acoustic waves to produce local shear-layer growth rates that are approximately 50% higher than the natural, smooth-walled baseline case. The conditions for optimum growth rates are in general concurrence with numerical predictions,In this study the how physics of a compressible shear layer in a wavy-wall environment was investigated with mean and fluctuating flowfield measurements, as well as schlieren visualizations.
引用
收藏
页码:1871 / 1878
页数:8
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