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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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