An experimental study at moderate and high subsonic speeds of the flow over wings with 30 degrees and 45 degrees of sweepback in conjunction with a fuselage

Author: Whitcomb, Richard T
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L50K27
Link: https://digital.library.unt.edu/ark:/67531/metadc58695/

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