Free-Flight Determination of Boundary-Layer Transition and Heat Transfer for a Hemisphere-Cylinder at Mach Numbers to 5.6

Author: Krasnican, M. J.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E57F10
Link: https://digital.library.unt.edu/ark:/67531/metadc63610/

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