Here we discuss the computational modeling of the receptivity of the laminar boundary layer on a semi-infinite flat plate with an elliptic leading edge. The incompressible flow is computed in a spatial simulation using the full Navier-Stokes equations in general curvilinear coordinates. Finite differences are used in both space directions and in time. First, the steady basic state is obtained in a transient approach using spatially varying time steps. Then, small-amplitude acoustic disturbances of the freestream velocity are applied as unsteady boundary conditions, and the governing equations are solved time-accurately to evaluate the spatial and temporal developments of instability waves (Tollmien-Schlichting waves) in the boundary layer. A sharper leading edge is found to be less receptive to freestream disturbances.
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Boundary Layer Receptivity to Sound: Navier-Stokes Computations
H. L. Reed,
H. L. Reed
Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106
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N. Lin,
N. Lin
Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106
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W. S. Saric
W. S. Saric
Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106
Search for other works by this author on:
H. L. Reed
Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106
N. Lin
Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106
W. S. Saric
Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ 85287-6106
Appl. Mech. Rev. May 1990, 43(5S): S175-S180
Published Online: May 1, 1990
Article history
Online:
April 30, 2009
Citation
Reed, H. L., Lin, N., and Saric, W. S. (May 1, 1990). "Boundary Layer Receptivity to Sound: Navier-Stokes Computations." ASME. Appl. Mech. Rev. May 1990; 43(5S): S175–S180. https://doi.org/10.1115/1.3120798
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