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Adjoint-Based Geometrically Constrained Aerodynamic Optimization of a Transonic Compressor Stage

Crossref DOI link: https://doi.org/10.1007/s11630-019-1141-5

Published Online: 2019-08-28

Published Print: 2019-10

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

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