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Published in 2019 at "Journal of Mechanical Science and Technology"
DOI: 10.1007/s12206-019-1046-y
Abstract: Significant unsteady film cooling performance of a turbine shroud can be found under the periodic disturbance of rotor blades. The mainstream flow in film cooling on a turbine shroud is simplified as the periodic swing…
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Keywords:
film cooling;
mainstream swing;
cooling performance;
film ... See more keywords
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0
Published in 2021 at "Aerospace Science and Technology"
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…
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Keywords:
film cooling;
inlet;
inlet non;
non uniformities ... See more keywords