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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