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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