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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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