University of North Texas Digital Library (University of North Texas) · 1948 · 17 citations · 2 references
Open access
EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsAerospace MaterialsAerospace StructuresAerodynamic DesignAerodynamic TestingAirfoil TheoryExperimental AerodynamicsWind-tunnel TestingAirfoil AerodynamicsAirfoil DesignCamber EffectsFlow Over AirfoilsHigh-mach-number AerodynamicsMach NumberMach Number EffectsThickness Effects
Report presenting an investigation to determine the aerodynamic characteristics of a group of NACA 16-series airfoils related in camber and thickness over a range of Mach numbers. All of the currently available force-test data for NACA 16-series airfoils obtained under the same test conditions in the 24-inch high-speed tunnel are presented.
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