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Transonic airfoil design and optimisation by using vibrational genetic algorithm

dc.contributor.authorHacıogˇlu, Abdurrahman
dc.contributor.authorÖzkol, I˙brahim
dc.date.accessioned2026-01-25T05:30:33Z
dc.date.issued2003-08-01
dc.description.abstractIn this study, the power of vibrational genetic algorithm (VGA) for transonic airfoil design and optimisation problems, which are generally characterized by multi‐model topology in the design parameter space, has been introduced. This type of problem is characterized by search and computational time to achieve satisfying solutions. In order to obtain more robust and faster algorithm, vibration concept, our earlier study, is further developed. This developed VGA is coupled with a full potential flow‐field solver for inverse design and airfoil optimisation problem in transonic case. The performance of this implemented strategy is compared with that offered by a classical or more commonly used genetic algorithm.
dc.description.urihttps://doi.org/10.1108/00022660310484275
dc.description.urihttps://dx.doi.org/10.1108/00022660310484275
dc.identifier.doi10.1108/00022660310484275
dc.identifier.endpage357
dc.identifier.issn0002-2667
dc.identifier.openairedoi_dedup___::6cf11db70cbc30986df8cc203019e933
dc.identifier.startpage350
dc.identifier.urihttps://hdl.handle.net/11527/46996
dc.identifier.volume75
dc.language.isoeng
dc.publisherEmerald
dc.relation.ispartofAircraft Engineering and Aerospace Technology
dc.rightsCLOSED
dc.titleTransonic airfoil design and optimisation by using vibrational genetic algorithm
dc.typeArticle
dspace.entity.typePublication

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