Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines
Figure 25
Spatially averaged Nusselt number ratio variations as dependent upon rotation number for the rotating channel investigation of Zhou and Acharya [102]. (a) Radial outflow pressure side results. (b) Radial outflow suction side results. (c) Radial inflow pressure side results. (d) Radial inflow suction side results.
