Show simple item record

dc.contributor.authorMaher N. Bismarck-Nasr
dc.date.accessioned2017-05-08T23:37:15Z
dc.date.available2017-05-08T23:37:15Z
dc.date.copyrightDecember, 1992
dc.date.issued1992
dc.identifier.issn0003-6900
dc.identifier.otherAMREAD-25636#461_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/109549
dc.description.abstractA review of the finite element method applied to the problem of supersonic aeroelastic stability of plates and shells is presented. The review is limited to linear models. Some new contributions in the field are presented and future trends are discussed.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleFinite Element Analysis of Aeroelasticity of Plates and Shells
dc.typeJournal Paper
dc.journal.volume45
dc.journal.issue12
dc.journal.titleApplied Mechanics Reviews
dc.identifier.doi10.1115/1.3119783
dc.journal.fristpage461
dc.journal.lastpage482
dc.identifier.eissn0003-6900
dc.keywordsAeroelasticity
dc.keywordsFinite element analysis
dc.keywordsPlates (structures)
dc.keywordsShells
dc.keywordsStability AND Finite element methods
dc.treeApplied Mechanics Reviews:;1992:;volume( 045 ):;issue: 012
dc.contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record