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Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of the NACA 653-418, a=1.0 Airfoil Section
Author:
Quinn, John H., Jr.
Year:
1945
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-82, NACA-CB-L5J04
Link:
https://digital.library.unt.edu/ark:/67531/metadc61407/
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