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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

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Distribution of Static Temperature in Secondary Air System and Blade Passage in a Meridional Plane

Velocity Field Near Rim

Streamlines in Cavity

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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

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