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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