Endwall Film-Cooling in Axial Flow Turbines
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چکیده
منابع مشابه
The Influence of Step and Fillet Shape on Nozzle Endwall Heat Transfer
Abstract—There is a gap at combustor-turbine interface where leakage flow comes out to prevent hot gas ingestion into the gas turbine nozzle platform. The leakage flow protects the nozzle endwall surface from the hot gas coming from combustor exit. For controlling flow’s stream, the gap’s geometry is transformed by changing fillet radius size. During the operation, step configuration is occurre...
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