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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