Two-dimensional wind-tunnel investigation of an approximately 14-percent-thick NACA 66-series-type airfoil section with a double slotted flap

Author: Braslow, Albert L.
Year: 1946
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1110
Link: https://digital.library.unt.edu/ark:/67531/metadc54964/

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