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Numerical study of combining steady Vortex Generator Jets and Deflected Trailing edge to reduce the blade numbers of low pressure turbine stage

Crossref DOI link: https://doi.org/10.1007/s11630-016-0892-5

Published Online: 2016-11-11

Published Print: 2016-12

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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