RESPONSE OF THE CAVITY SHEAR-LAYER OSCILLATIONS TO EXTERNAL FORCING

被引:46
作者
GHARIB, M
机构
[1] California Inst of Technology,, Pasadena, CA, USA, California Inst of Technology, Pasadena, CA, USA
关键词
AERODYNAMICS; -; Drag;
D O I
10.2514/3.9576
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Influence of externally forced initial flow conditions on axisymmetric cavity shear layer was studied. A sinusoidally heated strip upstream of the cavity excited Tollmien-Schlichting waves that, after amplification by the boundary layer, were introduced to the cavity shear layer. It is shown that by selecting a forcing frequency, which satisfies a phase difference criterion between two corners of the cavity and has an amplitude that is above the threshold amplitude, it is possible to excite a naturally nonoscillating shear layer. It is also shown that the frequency and amplitude of the oscillation in the self sustained mode can be controlled through external forcing. By using a feed-back control scheme, up to 40% reduction of the velocity fluctuation level can be obtained.
引用
收藏
页码:43 / 47
页数:5
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