Pressure Distributions Over a Wing-Fuselage Model at Mach Numbers of 0.4 to 0.99 and at 1.2

Author: Matthews, Clarence W.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L8H06
Link: https://digital.library.unt.edu/ark:/67531/metadc57953/

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