The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45 Degrees of Sweepback, an Aspect Ratio of 3, and a Taper Ratio of 0.5

Author: Kolbe, Carl D.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A51G31
Link: https://digital.library.unt.edu/ark:/67531/metadc58879/

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