Boundary-layer measurements in 3.84- by 10-inch supersonic channel

Paul F. Brinich
naca-tn-2203
Oct 1950


Boundary-layer measurements were made in the transonic and supersonic regions of a channel having maximum cross-sectional dimensions 3.84 by 10 inches and designed by potential-flow methods for a uniform Mach number of 2.08 in the test section.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1950/naca-tn-2203.pdf