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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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