Effects of systematic changes of trailing-edge angle and leading-edge radius on the variation with Mach number of the aerodynamic characteristics of a 10-percent-chord-thick NACA airfoil section
Description:
Report presenting the results of a wind-tunnel investigation of the effects of variation of trailing-edge angle and leading-edge radius on the aerodynamic characteristics of a 10-percent-chord-thick airfoil section at a range of Mach numbers.
Date:
September 26, 1949
Creator:
Summers, James L. & Graham, Donald J.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department