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Downwash Behind a Triangular Wing of Aspect Ratio 3 - Transonic Bump Method
Author:
Axelson, John A.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A53I23
Link:
https://digital.library.unt.edu/ark:/67531/metadc59879/
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