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Aircraft Air Inlet Design Optimization via Surrogate-Assisted Evolutionary Computation

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Part of the book series: Lecture Notes in Computer Science ((LNTCS,volume 9019))

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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Correspondence to Andre Lombardi .

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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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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-15891-4

  • Online ISBN: 978-3-319-15892-1

  • eBook Packages: Computer ScienceComputer Science (R0)

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