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Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8
Author:
Crawford, Davis H.
Year:
1956
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3706
Link:
https://digital.library.unt.edu/ark:/67531/metadc55989/
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