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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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