Aerofoil Theory of a Flat Delta Wing at Supersonic Speeds Open PDF Document Details Document Type Technical Report Publication Date Sep 01, 1946 Accession Number ADA800699 Entities People Amy K. Robinson Organizations Royal Aircraft Establishment Tags Communities of Interest Air Platforms DTIC Thesaurus Topics Aircrafts Airfoils Aspect Ratio Delta Wings Differential Equations Equations Flow Fluid Dynamics Fluid Flow Free Stream Leading Edges Mach Number Mechanics Pressure Distribution Scalar Functions Subsonic Flow Two Dimensional Technology Areas Hypersonics Hypersonics - Hypersonic Flow