ME53300 - Turbomachinery 2
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.
Credit Hours: 3
Instructor(s): Guillermo Paniagua-Perez
Phone: (765) 494-1514
Other Phone: (765) 404-7747
Email: gpaniagua@purdue.edu
Office: Zucrow Labs ZL3
Web: Instructor Homepage
Learning Objective:
- Design a turbomachine, assess their aerodynamic performance & and convective heat transfer
- Characterize the unsteady behavior of the turbomachinery, forced response, noise
- Communicate final developed design to a panel of experts in the field
- Develop a critical analysis to optimize future turbomachinery concepts based on physical principles
- Outline future research programs to address aerothermal challenges
Description:
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.
Applied / Theory:
50 / 50