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dc.contributor.authorXiao, Yang
dc.contributor.authorZhang, Yufei
dc.date.accessioned2026-08-20T21:12:22Z
dc.date.available2026-08-20T21:12:22Z
dc.date.copyright2025/08/12
dc.date.issued2025
dc.identifier.otherJAEEEZ.ASENG-5602.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314111
dc.description.abstractAbstractThe aerodynamic shape optimization of air-breathing hypersonic vehicles often involves a high computational load due to the large number of design variables. Additionally, the complex shockwave structures and shockwave-geometry interactions can ...
dc.publisherAmerican Society of Civil Engineers
dc.titleAerodynamic Shape Optimization of Forebodies Based on the GEK and Discrete Adjoint Methods
dc.typeJournal Article
dc.journal.volume38
dc.journal.issue6
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-5602
dc.journal.fristpage04025086-1
dc.journal.lastpage04025086-15
dc.page15
dc.treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006
dc.contenttypeFulltext


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