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Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9
Report presenting an investigation of the Reynolds number for transition on the outside of a hollow cylinder with heat transfer from the boundary layer to the wall at Mach number 6.9. At a given Mach number, it appears that the Reynolds number based on leading-edge thickness is an important parameter in comparisons of flat-plate transition data from various installations.
Date:
February 9, 1956
Creator:
Bertram, Mitchel H.
System:
The UNT Digital Library