Stability of the Supersonic Laminar Boundary Layer With a Pressure Gradient Open PDF Document Details Document Type Technical Report Publication Date Nov 20, 1950 Accession Number ADA800183 Entities People Lester Lees Organizations Princeton University Tags Communities of Interest Advanced Electronics Air Platforms Materials and Manufacturing Processes DTIC Thesaurus Topics Aerodynamic Heating Boundary Layer Boundary Layer Flow Computational Fluid Dynamics Differential Equations Equations Fluid Dynamics Heat Transfer Laminar Boundary Layer Leading Edges Mach Number Perturbation Theory Pressure Distribution Pressure Gradients Reynolds Number Steady Flow Turbulent Flow Technology Areas Hypersonics Hypersonics - Hypersonic Boundary Layers