Numerical study on unsteady film cooling performance of turbine rotor considering influences of inlet non-uniformities and upstream coolant
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DOI: 10.1016/j.ast.2021.107089
Abstract: Abstract High-pressure turbine (HPT) rotor blades work in a harsh environment with high temperature and rotational speed. Affected by blade row interaction and inlet non-uniformities, the rotor flow field behaves with significant unsteady characteristics. In… read more here.
Keywords: film cooling; inlet; inlet non; non uniformities ... See more keywords