Remarks concerning the behavior of the laminar boundary layer in compressible flows

Neal Tetervin
Jan 1949

The boundary-layer equation of motion and the boundary-layer energy equation for the compressible and steady laminar boundary-layer on two-dimensional bodies and bodies of revolution are written in a nondimensional form to provide a clearer indication of the effects of Mach number, Reynolds number, and the properties of the gas.

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