Some Effects of Fin Leading-Edge Shape on Aerodynamic Heating at Mach Number 2.0 at a Stagnation Temperature of About 2,600 Degrees R

Author: Bland, William M., Jr.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57K12
Link: https://digital.library.unt.edu/ark:/67531/metadc63860/

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