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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