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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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