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Adjoint Optimization of a Centrifugal Compressor Impeller for Turbochargers
ターボチャージャ用遠心圧縮機インペラを対象としたAdjoint最適化
2021
Turbomachinery
ターボチャージャ用遠心圧縮機インペラを対象としたAdjoint最適化
Design optimization have become widely used in industry fields as a means of improving aerodynamic performance while satisfying various design constraints. Adjoint method, which can calculate the sensitivity of the objective improvement to shape changes by only one calculation, has been adapted gradient-based optimizations to reduce the calculation cost. In this study, single-point and multi-points gradient-based optimizations using adjoint method were conducted for a centrifugal compressor
doi:10.11458/tsj.49.10_577
fatcat:d5zqt2qhx5hulbbqrapobx2ida