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Data From Large-Scale Low-Speed Tests of Airplane Configurations With a Thin 45 Degree Swept-Wing Incorporating Several Leading-Edge Contour Modifications
Author:
Evans, William T.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A56B17
Link:
https://digital.library.unt.edu/ark:/67531/metadc62415/
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