Uncertainty quantification of the effects of squealer tip geometry deviation on aerothermal performance
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DOI: 10.1177/0957650919898617
Abstract: The first-stage rotor squealer tip is a key area in gas turbine for both aerodynamic performance and blade cooling tasks, which should be carefully designed. However, harsh operating conditions near the rotor squealer tip can… read more here.
Keywords: geometry; squealer tip; aerothermal performance;