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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