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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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