Effect of wear damage on aero-thermal performance of the film-cooled squealer tip in a turbine stage
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DOI: 10.1177/09576509231171424
Abstract: Effects of wear damage on the aerodynamic performance, heat transfer and film cooling effect in the squealer tip region of a gas turbine stage were investigated under engine condition. Two wear parameters, including the starting-location… read more here.
Keywords: turbine stage; film; stage; wear damage ... See more keywords