THE FLAT DELTA WING AT INCIDENCE, AT SUPERSONIC SPEEDS, WHEN THE LEADING EDGES LIE OUTSIDE THE MACH CONE OF THE VERTEX

Abstract

H. J. Stewart's (1) analysis using the linearized equation of supersonic flows for finding the lift of a flat delta wing at supersonic speeds when the leading edges of the wing lie within the Mach cone of the vertex, is extended to the case when the leading edges of the wing lie outside the Mach cone of the vertex.