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Steady RANS CFD solver suffers from convergence difficulty when analyzing turbomachinery flows at off-design conditions, such as stall. A strong CFD solver based on the Newton-Krylov method is developed to improve the convergence for such conditions.

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This page is a summary of: Newton–Krylov Solver for Robust Turbomachinery Aerodynamic Analysis, AIAA Journal, March 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058523.
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