Effects of Reynolds number on the aerodynamic characteristics of a delta wing at Mach number of 2.41

Author: Hatch, John E , Jr
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51H06
Link: https://digital.library.unt.edu/ark:/67531/metadc58969/

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