Drag Tests of an NACA 65(215)-114, a = 1.0 Practical-Construction Airfoil Section Equipped with a 0.295-Airfoil-Chord Slotted Flap

Author: Quinn, John H., Jr.
Year: 1947
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1236
Link: https://digital.library.unt.edu/ark:/67531/metadc55181/

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