A flight investigation of the boundary-layer characteristics and profile drag of the NACA 35-215 laminar-flow airfoil at high Reynolds numbers

Author: Platt, Robert C.
Year: 1941
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-532, NACA-MR
Link: https://digital.library.unt.edu/ark:/67531/metadc61113/

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