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This thesis presents a shape optimization approach for turbomachinery applications using the adjoint method and accurate equations of state to model real gas effects. The numerical tools developed include flow and adjoint solvers, as well as algorithms for shape parameterization, mesh deformation, and optimization. The potential of the approach is demonstrated on 2D aerodynamic and turbomachinery design problems, including re-designing a wind tunnel nozzle and optimizing cascades for transonic and supersoni

Author

Vidushee Geetam

Language

EN