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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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