Aerodynamic heating of a wing as determined from a free-flight rocket-model test to Mach number 3.64

Author: Swanson, Andrew G.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56F11a
Link: https://digital.library.unt.edu/ark:/67531/metadc62723/

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