ME 53300 - Turbomachinery II

Credit Hours: 3.00. Aerodynamic analysis and design of axial flow and radial flow gas compressors and gas turbines. Blade element performance (deflection, profile and shock losses, etc.). Meridional flow analysis for general radial equilibrium. Secondary flow and end-wall boundary layer models. Centrifugal compressor modeling. Unsteady flow, rotating stall, and surge. Typically offered Spring.