2023
DOI: 10.1016/j.engappai.2023.106192
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Engineering applications of multi-objective evolutionary algorithms: A test suite of box-constrained real-world problems

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Cited by 17 publications
(6 citation statements)
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“…In this part, the effectiveness of NLDEA was further verified in the practical problem of unconstrained and irregular PF, that is, water and oil repellent fabric development (WORFD) (Ahmad et al, 2017;Zapotecas-Martínez et al, 2023). The textile industry aims to create high-value fabrics, often achieving hydrophobicity, or water and oil repellency, through various process parameters (Sun et al, 2005).…”
Section: Application To Real-world Problemsmentioning
confidence: 99%
“…In this part, the effectiveness of NLDEA was further verified in the practical problem of unconstrained and irregular PF, that is, water and oil repellent fabric development (WORFD) (Ahmad et al, 2017;Zapotecas-Martínez et al, 2023). The textile industry aims to create high-value fabrics, often achieving hydrophobicity, or water and oil repellency, through various process parameters (Sun et al, 2005).…”
Section: Application To Real-world Problemsmentioning
confidence: 99%
“…In order to address the challenges posed by artificial test problems, several real-world test suites [1], [34] have been proposed in the literature, predominantly comprising singleand multi-objective problems. Nevertheless, there has been a lack of literature addressing the development of a comprehensive test suite designed explicitly for many-objective optimization real-world problems.…”
Section: A Motivationsmentioning
confidence: 99%
“…These objectives are: minimizing the distance VOLUME 10, 2022 from the inlet combustion (D cc ), the maximum temperature at injector surface (T Smax ), maximum temperature at the injector post tip (T Pmax ), and temperature at three inches from the injector surface (T is ). In addition to these four objectives, the liquid-rocket singleelement injector design problem involves three decision variables that describe crucial design parameters: the angle at which hydrogen flows, the proportional increase in the hydrogen area relative to the standard cross-sectional area of the tube carrying hydrogen, and the proportional decrease in the oxygen area concerning the standard cross-sectional area of the tube carrying oxygen, as described in [1]. Therefore, the liquid-rocket single-element injector design problem is formulated as…”
Section: Real-world Many-objective Test Suitementioning
confidence: 99%
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