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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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