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An Experimental Investigation of the Zero-Lift-Drag Characteristics of Symmetrical Blunt-Trailing-Edge Airfoils at Mach Numbers From 2.7 to 5.0
Author:
Syvertson, Clarence A.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A53B02
Link:
https://digital.library.unt.edu/ark:/67531/metadc59776/
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