Journal of Fluid Mechanics · 1996 · 45 citations · 19 references
Natural SciencesAerospace EngineeringPhysicsAcousticsComputational Fluid DynamicsFluid DynamicsAcoustic Wave PropagationBoundary Layer EffectsBoundary Layer FlowBoundary LayersBoundary-layer TheoryPhysical AcousticsAcoustic Wave EquationsAcoustic WavesFlat Plate Boundary LayersMach NumberMach Number EffectsReynolds NumberReynolds Number EffectsStrouhal Number
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 = ω r n / U , where ω 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 flat 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.
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Handbook of Mathematical Functions
Donald A. McQuarrie · American Journal of Physics · 1966 · 40.9K citations
Perturbation Methods in Fluid Mechanics
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Methods Based on the Wiener-Hopf Technique.
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