Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers From 1.90 to 3.07

Author: O'Neal, Robert L.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L58A13
Link: https://digital.library.unt.edu/ark:/67531/metadc63727/

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