INDUSTRIAL MULTI-FIDELITY SURROGATE-BASED OPTIMIZATION FRAMEWORK FOR COMPRESSOR BLADE DESIGN: BALANCING AEROMECHANICS, CONTACT ROBUSTNESS, AND NI-POD MODELING
This paper presents the improvements of a modular, multi-disciplinary, and multi-fidelity Surrogate-Based Optimization (SBO) framework for rotor blade design, aiming at reducing computational cost and accelerating the design process in aeromechanical applications. The concept of “useful accuracy” is central to our ap...