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Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees
Author:
Stivers, Louis S , Jr
Year:
1954
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3162
Link:
https://digital.library.unt.edu/ark:/67531/metadc57054/
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