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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-A54B16
Link:
https://digital.library.unt.edu/ark:/67531/metadc60142/
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