On the Laminar Boundary Layer Separation from the Leading Edge of a Thin Aerofoilv Open PDF Document Details Document Type Technical Report Publication Date Oct 01, 1953 Accession Number ADB952994 Entities People L. Klanfer P. R. Owen Tags Communities of Interest Air Platforms DTIC Thesaurus Topics Aircrafts Airfoils Boundary Layer Boundary Layer Flow Flow Fluid Dynamics Laminar Boundary Layer Layers Leading Edges Military Aircraft Pressure Distribution Reynolds Number Shock Waves Sweptback Wings Turbulent Mixing Two Dimensional Wind Tunnels