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/metadc64262/

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