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Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design

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dc.contributor.authorDemiroglu, Yusuf
dc.contributor.authorYildiz, Sihmehmet
dc.contributor.authorNikbay, Melike
dc.date.accessioned2026-01-24T17:48:34Z
dc.date.issued2021-01-04
dc.description.urihttps://doi.org/10.2514/6.2021-1009
dc.description.urihttps://dx.doi.org/10.2514/6.2021-1009
dc.identifier.doi10.2514/6.2021-1009
dc.identifier.openairedoi_dedup___::1cd432e8a592d4e85faa43fc5b04f396
dc.identifier.orcid0000-0002-6444-0262
dc.identifier.orcid0000-0001-5447-172x
dc.identifier.urihttps://hdl.handle.net/11527/36530
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)
dc.relation.ispartofAIAA Scitech 2021 Forum
dc.titleMulti-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design
dc.typeArticle
dspace.entity.typePublication

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