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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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