Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling

Ivan E. Beckwith
naca-tn-4345
Sep 1958


Heat-transfer and skin-friction parameters obtained from exact numerical solutions to the laminar compressible-boundary-layer equations for the infinite cylinder in yaw are presented. The chordwise flow in the transformed plane is of the Falkner-Skan type. Solutions are given for chordwise stagnation flow with both a porous and a nonporous wall.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1958/naca-tn-4345.pdf