A transonic-wing investigation in the Langley 8-foot high-speed tunnel at high subsonic Mach numbers and at a Mach number of 1.2 : wing-fuselage configuration having a wing of 60 degree sweepback, aspect-ratio 4, taper ratio 0.6, and NACA 65A006 airf

Author: Wood, Raymond B
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L50J25
Link: https://digital.library.unt.edu/ark:/67531/metadc58621/

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