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- W596210874 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." @default.
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- W596210874 date "2015-01-01" @default.
- W596210874 modified "2023-10-16" @default.
- W596210874 title "Aircraft Air Inlet Design Optimization via Surrogate-Assisted Evolutionary Computation" @default.
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- W596210874 doi "https://doi.org/10.1007/978-3-319-15892-1_21" @default.
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