Show simple item record

dc.contributor.authorTrivedi, Madhu
dc.contributor.authorBakshi, Kaustav
dc.date.accessioned2026-08-20T21:14:08Z
dc.date.available2026-08-20T21:14:08Z
dc.date.copyright2025/08/19
dc.date.issued2025
dc.identifier.otherJAEEEZ.ASENG-6374.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314158
dc.description.abstractAbstractIn the literature, free vibration studies of skewed elliptical paraboloidal panels with composite stiffeners are missing, especially using geometric nonlinearity. This paper fills that deficiency. It proposes a C0 finite-element formulation that ...Practical ApplicationsThe body panels of aircraft and spacecraft are fabricated using doubly curved panels. The wings, ailerons, elevator, flaps, rotor blades, and doors of landing gear are the practical examples. These parts are generally made of ...
dc.publisherAmerican Society of Civil Engineers
dc.titleGeometrically Nonlinear Free Vibration of Composite Skewed Stiffened Elliptic Paraboloidal Panels
dc.typeJournal Article
dc.journal.volume38
dc.journal.issue6
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6374
dc.journal.fristpage04025087-1
dc.journal.lastpage04025087-18
dc.page18
dc.treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006
dc.contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record