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

Neal Tetervin
naca-tn-1805
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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1949/naca-tn-1805.pdf