BOUNDARY-LAYER RECEPTIVITY TO FREESTREAM DISTURBANCES

By W. Saric, H. Reed, E. Kerschen. 2002

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Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels (2013, background): “The receptivity mechanisms by which the disturbances enter a boundary layer are influenced by ablation, roughness, waviness, bluntness, curvature, Mach number, and so on [2].”
Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers (2012, background): “In general, transition is a result of the nonlinear response of a laminar boundary layer to various environmental disturbances (Saric et al. 2002).”
Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances (2005, background): “To quantitatively study the acoustic receptivity of the second mode, the receptivity can be measured by a branch I receptivity coefficient (Saric et al. 2002) defined as the ratio of the induced second-mode amplitude at the branch I neutral stability”
Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound (2003, methodology): “receptivity coefficient used in the literature (Saric et al. 2002), they are termed the response coefficients in this paper.”