Thermal performance improvement on winglet tip of a turbine stage under engine condition-part I: Winglet geometry modifications
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DOI: 10.1177/09576509221122035
Abstract: Heat transfer and film cooling effect on the winglet-squealer tip in the first stage of a gas turbine were numerically investigated under engine condition. To reveal the effect of P.S. (pressure side) winglet geometry on… read more here.
Keywords: geometry; winglet tip; tip; winglet geometry ... See more keywords