Tests of a Heated Low-Drag Airfoil
Description:
Report discusses the results of an experimental investigation into the NACA 65,2-016 heated wing. Information about the effect of heating on the drag coefficients, Reynolds numbers, and stability of the laminar boundary layer.
Date:
December 1942
Creator:
Frick, Charles W., Jr. & McCullough, George B.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department