CCS and Power Systems
Advanced Energy Systems - Hydrogen Turbines
Analysis of Gas Turbine Thermal Performance
Performer: Ames National Laboratory
Project No: FWP-AL05205018
Figure 1. Schematic of the wedge-shaped duct with ribs and pin fins for the trailing edge of a turbine vane/blade.
Figure 2. Streamlines showing how the ribs turn radially outward flow towards the axial direction.
Figure 3. Heat Flux on the Wall Induced by Pin Fins as obtained by using the following turbulence models: realizable k-ε, shear-stress transport (SST), and full Reynolds stress model (RSM) with stress-omega in the near-wall region.