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The Development of Cambered Airfoil Sections Having Favorable Lift Characteristics at Supercritical Mach Numbers
Author:
Graham, Donald J
Year:
1948
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1771
Link:
https://digital.library.unt.edu/ark:/67531/metadc55024/
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