Abstract
In aviation, the performance impact of auxiliary air inlets used for system ventilation is significant. The flow phenomena and consequently the numerical model, is highly non-linear, leading to a compromise between pressure recovery and drag for a given mass flow condition. This work follows a step-by-step approach which highlights the important issues related to solving such complex optimization problem, using surrogate methods coupled to evolutionary algorithms. Its conclusions can be used as a guideline to similar industrial applications.
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© 2015 Springer International Publishing Switzerland
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Lombardi, A., Ferrari, D., Santos, L. (2015). Aircraft Air Inlet Design Optimization via Surrogate-Assisted Evolutionary Computation. In: Gaspar-Cunha, A., Henggeler Antunes, C., Coello, C. (eds) Evolutionary Multi-Criterion Optimization. EMO 2015. Lecture Notes in Computer Science(), vol 9019. Springer, Cham. https://doi.org/10.1007/978-3-319-15892-1_21
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DOI: https://doi.org/10.1007/978-3-319-15892-1_21
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