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Wing-tunnel investigation at Mach numbers from 0.50 to 1.29 of an all-movable triangular wing of aspect ratio 4 alone and with a body
Author:
Stivers, Louis S.
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A9L01
Link:
https://digital.library.unt.edu/ark:/67531/metadc58401/
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