1955•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Wing pressure distributions over the lift range of the convair xf-92a delta-wing airplane at subsonic and transonic speeds
Earl R Keeener, Gareth H Jordan
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Abstract
Report presenting chordwise pressure distributions measured over the left wing of the Convair XF-92A delta-wing airplane to determine the effect of lift on the wing characteristics at subsonic and transonic Mach numbers. Results regarding the chordwise pressure distributions, wing-section aerodynamic characteristics, spanwise distribution, and elevon-section loads are provided.