Investigation of wing-tip ailerons on a 51.3 degrees sweptback wing at transonic speeds by the transonic-bump method

Author: Moseley, William C., Jr.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51H27
Link: https://digital.library.unt.edu/ark:/67531/metadc59086/

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