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Wind-Tunnel Investigation at Low Speed of a Wing Swept-Back 63 Degrees and Twisted and Cambered for a Uniform Load at a Lift Coefficient of 0.5
Author:
Weiberg, James A.
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A50A23
Link:
https://digital.library.unt.edu/ark:/67531/metadc58464/
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