The turbulent boundary layer with variable Prandtl number.

Mode of access: Internet.

Hypersonic flow with combined leading-edge bluntness and boundary-layer displacement effect.

"This report is based on research sponsored by the U. S. Navy through the Office of Naval Research, Contract Nonr-2653(00)."

Pressure gradient effects on supersonic boundary layer turbulence : final report /

"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation."

M=3 turbulent boundary layer measurements at very high Reynolds numbers /

"Interim report for period January 1975 to September 1976."