Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50- airfoil chord plain sealed flaps

Author: Brewer, Jack D.
Year: 1948
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1574
Link: https://digital.library.unt.edu/ark:/67531/metadc54904/

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