Measurements of Heat Transfer and Boundary-Layer Transition on an 8-inch-Diameter Hemisphere-Cylinder in Free Flight for a Mach Number Range of 2.00 to 3.88.

Garland, Benjamine J., Chauvin, Leo T.
naca-rm-l57d04a
April 1957


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-l57d04a.pdf