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Path optimization for multi-axis EDM drilling of combustor liner cooling holes using SCGA algorithm



Effect of geometric modification on flow behaviour and performance of reverse flow combustor



A REVIEW OF HEAT TRANSFER AND PRESSURE LOSS CHARACTERISTICS THROUGH CONVECTIVE COOLING METHOD FOR GAS TURBINE THERMAL MANAGEMENT


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10.1016/J.IJHEATMASSTRANSFER.2018.11.067

Heat transfer and pressure loss of turbulent flow in channels with miniature structured ribs on one wall


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Combustor Liners 연소기 라이너
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