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Chordwise Pressure Distributions on a 12-Foot-Span Wing of NACA 66-Series Airfoil Sections Up to a Mach Number of 0.60
Author:
Wall, Nancy E.
Year:
1948
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1696
Link:
https://digital.library.unt.edu/ark:/67531/metadc54796/
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