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The Characteristics of 78 Related Airfoil Sections from Tests in the Variable-Density Wind Tunnel

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460. NACA, (1933)

Abstract

An investigation of a large group of related airfoils was made in the NACA variable-density wind tunnel at a large value of the Reynolds number. The tests were made to provide data that may be directly employed for a rational choice of the most suitable airfoil section for a given application. The variation of the aerodynamic characteristics with variations in thickness and mean-line form were systematically studied.

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