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Full-Scale Investigation of a Wing With the Leading Edge Swept Back 47.5 Degrees and Having Circular-Arc and Finite-Trailing-Edge-Thickness Ailerons
Author:
Lange, Roy H.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9B02
Link:
https://digital.library.unt.edu/ark:/67531/metadc58272/
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