Investigation at transonic speeds of loading over a 30 degree sweptback wing of aspect ratio 3, taper ratio 0.2, and NACA 65A004 airfoil section mounted on a body

Author: Arabian, Donald D.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57G09a
Link: https://digital.library.unt.edu/ark:/67531/metadc63568/

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