Theoretical and Experimental Investigation of Aerodynamic-Heating and Isothermal Heat-Transfer Parameters on a Hemispherical Nose With Laminar Boundary Layer at Supersonic Mach Numbers

Author: Stine, Howard A.
Year: 1954
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3344
Link: https://digital.library.unt.edu/ark:/67531/metadc57545/

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