Gas Turbine Cooling & Secondary Air System
Cooling of Blades and Further Component Parts
Conjugate Heat Transfer
Secondary Air Flow in Interaction with Blade Passage Flow
Complex Wheel Space Geometries with Rim and Labyrinth Seals considering the Interaction of Stationary and Rotating Parts
Pre-Swirl Systems
Distribution of Static Temperature in Secondary Air System and Blade Passage in a Meridional Plane
Velocity Field Near Rim
Streamlines in Cavity
Blade Temperature Distribution
Heat Transfer Coefficient Distribution on Receiver Hole Walls
Heat Transfer Coefficient Distribution on Rotor Disk for Different Stator-Rotor Positions
Receiver Inlet Relative Temperature vs. Rotational Speed. Comparison of Predictions with Experiments
Pre-Swirl Discharge Coefficient vs. Rotational Speed. Comparison of Predictions with Experiments