Effect of a leading-edge flap upon the lift, drag, and pitching moment of an airplane employing a thin, unswept wing

Author: Heitmeyer, John C.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A54B16
Link: https://digital.library.unt.edu/ark:/67531/metadc60142/

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