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A Combined Experimental and Turbulence-Resolved Modeling Approach for Aeroengine Turbine Rim Seals
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Ingress is the penetration of hot mainstream gas into the rotor–stator wheel-space formed between adjacent disks; a rim seal is installed at the periphery of the wheel-space. Purge flow is bled from the compressor and ...