Wind-Tunnel Investigation at Low Speed of a Wing Swept Back 63 Degrees and Twisted and Cambered for Uniform Load at a Lift Coefficient of 0.5 and With a Thickened Tip Section

Author: Weiberg, James A.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A50I14
Link: https://digital.library.unt.edu/ark:/67531/metadc58676/

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