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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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