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dc.contributor.authorCrescenti, Fen
dc.contributor.authorKipouros, Timoleonen
dc.contributor.authorSavill, MAen
dc.date.accessioned2019-07-31T23:30:31Z
dc.date.available2019-07-31T23:30:31Z
dc.date.issued2018-01-01en
dc.identifier.isbn9781624105500en
dc.identifier.urihttps://www.repository.cam.ac.uk/handle/1810/295147
dc.description.abstract© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Topology optimization is a technique used to identify the optimal layout of a structure for a given objective and assigned boundary conditions. The progress it has experienced over the last three decades made it ready for industrial applications. In this paper topology optimization is employed to investigate the influence of sweep angle, aspect ratio and loading condition on the wing internal structure. The planform of the Common Research Model wing is used as a baseline. The geometry is modified parametrically to alter sweep angle and aspect ratio. Regarding the baseline planform, the optimization is performed considering the aerodynamic loading induced by the pull-up manoeuvre. Results are provided for AR = 7 and AR = 11, as well as sweep angle of 20 and 30 degrees. The results of topology optimization for all cases are compared. Common patterns are identified and exported to provide guidelines for the preliminary design of the wing primary structure.
dc.rightsAll rights reserved
dc.titleLoading and planform shape influence of the wing structural layout through topology optimizationen
dc.typeConference Object
prism.publicationDate2018en
prism.publicationName2018 Multidisciplinary Analysis and Optimization Conferenceen
dc.identifier.doi10.17863/CAM.42216
rioxxterms.versionofrecord10.2514/6.2018-3578en
rioxxterms.versionAM
rioxxterms.licenseref.urihttp://www.rioxx.net/licenses/all-rights-reserveden
rioxxterms.licenseref.startdate2018-01-01en
dc.contributor.orcidKipouros, Timoleon [0000-0003-3392-283X]
rioxxterms.typeConference Paper/Proceeding/Abstracten
rioxxterms.freetoread.startdate2019-01-01


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