1954•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Wind pressure distributions at low lift for the XF-92A delta-wing airplane at transonic speeds
E. R. Keener
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Abstract
Report presenting chordwise pressure distributions measured over the left wing of a Convair XF-92A delta-wing airplane at low lift to determine the effect of Mach number on the wing characteristics at transonic speeds. The critical Mach number of the basic wing was 0.83 for an airplane normal-force coefficient at 0.09. The spanwise load distributions were roughly triangular in shape.