Massoudi, SoheylPicard, CyrilSchiffmann, Jurg2022-01-312022-01-312022-01-312022-01-0610.1017/dsj.2021.25https://infoscience.epfl.ch/handle/20.500.14299/184879WOS:000739467800001Although robustness is an important consideration to guarantee the performance of designs under deviation, systems are often engineered by evaluating their performance exclusively at nominal conditions. Robustness is sometimes evaluated a posteriori through a sensitivity analysis, which does not guarantee optimality in terms of robustness. This article introduces an automated design framework based on multiobjective optimisation to evaluate robustness as an additional competing objective. Robustness is computed as a sampled hypervolume of imposed geometrical and operational deviations from the nominal point. In order to address the high number of additional evaluations needed to compute robustness, artificial neutral networks are used to generate fast and accurate surrogates of high-fidelity models. The identification of their hyperparameters is formulated as an optimisation problem. In the frame of a case study, the developed methodology was applied to the design of a small-scale turbocompressor. Robustness was included as an objective to be maximised alongside nominal efficiency and mass-flow range between surge and choke. An experimentally validated 1D radial turbocompressor meanline model was used to generate the training data. The optimisation results suggest a clear competition between efficiency, range and robustness, while the use of neural networks led to a speed-up by four orders of magnitude compared to the 1D code.Engineering, ManufacturingEngineeringrobust designrobustnesspredesignartificial neural networkshyperparameter tuningmultiobjective optimisationnsga-iiiradial compressorheat-pumpmicroturbomachinerynondominated sorting approachtext::journal::journal article::research article