A rigorous proof that subsonic boundary layer profiles are structurally stable for the steady compressible Navier-Stokes equations, plus a low Mach number limit with a Prandtl layer.
F.: Transition thresh old for the 2-D Couette flow in a finite channel
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Structural stability of boundary layers in the entire subsonic regime
A rigorous proof that subsonic boundary layer profiles are structurally stable for the steady compressible Navier-Stokes equations, plus a low Mach number limit with a Prandtl layer.