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Published in 2020 at "Journal of Aerospace Engineering"
DOI: 10.1061/(asce)as.1943-5525.0001095
Abstract: AbstractTo support the design of a two-dimensional turbine blade profile with reduced shock loss, an efficient model for shock system with separation shock in highly loaded turbine cascade needed t...
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Keywords:
turbine;
shock system;
turbine cascade;
highly loaded ... See more keywords