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Lift and pitching moment at low speeds of the naca 64A010 airfoil section equipped with various combinations of a leading-edge slat, leading-edge flap, split flap, and double-slotted flap
Author:
Kelly, John A.
Year:
1953
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3007
Link:
https://digital.library.unt.edu/ark:/67531/metadc56757/
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