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Wind-tunnel investigation of an NACA 23012 airfoil with a 30 percent chord Maxwell slate and with trailing-edge flaps
Author:
Lowry, John G.
Year:
1941
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-693, NACA-MR
Link:
https://digital.library.unt.edu/ark:/67531/metadc61443/
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