Boundary-layer receptivity for a parabolic leading edge

被引:37
作者
Hammerton, PW [1 ]
Kerschen, EJ [1 ]
机构
[1] UNIV ARIZONA,DEPT AEROSP & MECH ENGN,TUCSON,AZ
关键词
D O I
10.1017/S0022112096001796
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The effect of the nose radius of a body on boundary-layer receptivity is analysed for the case of a symmetric mean flow past a body with a parabolic leading edge. Asymptotic methods based on large Reynolds number are used, supplemented by numerical results. The Mach number is assumed small, and acoustic free-stream disturbances are considered. The case of free-stream acoustic waves, propagating obliquely to the symmetric mean flow is considered. The body nose radius, r(n), enters the theory through a Strouhal number, S = omega r(n)/U, where omega is the frequency of the acoustic wave and U is the mean flow speed. The finite nose radius dramatically reduces the receptivity level compared to that for a fiat plate, the amplitude of the instability waves in the boundary layer being decreased by an order of magnitude when S = 0.3. Oblique acoustic waves produce much higher receptivity levels than acoustic waves propagating parallel to the body chord.
引用
收藏
页码:243 / 267
页数:25
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