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A Wind-Tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds
Author:
Heath, Atwood R., Jr.
Year:
1958
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L58E12
Link:
https://digital.library.unt.edu/ark:/67531/metadc52884/
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