Simultaneous shape and topology optimization of wings

This paper presents a method for simultaneous optimization of the outer shape and internal topology of aircraft wings, with the objective of minimizing drag subject to lift and compliance constraints for multiple load cases. The physics are evaluated by the means of a source-doublet panel method for...

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Bibliographic Details
Published inarXiv.org
Main Authors Høghøj, Lukas C, Conlan-Smith, Cian, Sigmund, Ole, Casper Schousboe Andreasen
Format Paper Journal Article
LanguageEnglish
Published Ithaca Cornell University Library, arXiv.org 28.04.2023
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