STUDY OF THE FLOW OF A RADIATING GAS BY A DIFFERENTIAL APPROXIMATION Open PDF Document Details Document Type Technical Report Publication Date Jan 01, 1965 Accession Number AD0615597 Entities People Ping Cheng Organizations Stanford University Tags Communities of Interest Air Platforms Energy and Power Technologies DTIC Thesaurus Topics Air Force Boltzmann Equation Boundary Layer Computational Fluid Dynamics Computational Science Differential Equations Energy Transfer Fluid Dynamics Gas Flow Heat Transfer Mach Number Partial Differential Equations Physical Theories Plane Geometry Radiative Transfer Thermal Conductivity Two Dimensional