Boundary-layer development and skin friction at mach number 3.05

Paul F. Brinich, Nick S. Diaconis
naca-tn-2742
Jul 1952


Experimental and theoretical results are presented for boundary layer studies consisting of Schlieren observations and momentum surveys made on hollow cylinder models with their axes aligned parallel to the stream. Results were obtained for three model diameters and for natural and artificially induced turbulent boundary layer flows.

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