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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