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Aerodynamic heat transfer and zero-lift of a flat windshield canopy on the NACA RM-10 research vehicle at high Reynolds numbers for a flight Mach number range from 1.5 to 3.0
Author:
Hoffman, Sherwood
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56G05
Link:
https://digital.library.unt.edu/ark:/67531/metadc62520/
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