Wing-tunnel investigation at Mach numbers from 0.50 to 1.29 of an all-movable triangular wing of aspect ratio 4 alone and with a body

Author: Stivers, Louis S.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A9L01
Link: https://digital.library.unt.edu/ark:/67531/metadc58401/

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