Effects of Mach Number and Reynolds Number on the Maximum Lift Coefficient of a Wing of NACA 230-Series Airfoil Sections

Author: Furlong, G. Chester
Year: 1947
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1299
Link: https://digital.library.unt.edu/ark:/67531/metadc55257/

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