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-SA54B16
Link: https://digital.library.unt.edu/ark:/67531/metadc65592/

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