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Experimental Investigation of the Effects of Vortex Generators on the Maximum Lift of a 6-Percent-Thick Symmetrical Circular-Arc Airfoil Section
Author:
Bursnall, William J.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52G24
Link:
https://digital.library.unt.edu/ark:/67531/metadc59343/
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