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contributor authorD. H. Seitz
date accessioned2017-05-09T01:18:37Z
date available2017-05-09T01:18:37Z
date copyrightJune, 1972
date issued1972
identifier issn0021-8936
identifier otherJAMCAV-25961#495_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158156
description abstractA numerical method for stress analysis of three-layered, honeycomb-type sandwich plates and shells of arbitrary thickness is illustrated by application to a thick conical frustum. Results are demonstrated in a numerical example. The method features an exact elasticity analysis of the core including transverse shear and transverse normal stress. The facings are treated by classical shell theory. The numerical method used is forward integration.
publisherThe American Society of Mechanical Engineers (ASME)
titleExact Analysis of a Thick Sandwich Conical Shell by Forward Integration
typeJournal Paper
journal volume39
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3422706
journal fristpage495
journal lastpage500
identifier eissn1528-9036
keywordsShells
keywordsNumerical analysis
keywordsPlates (structures)
keywordsThickness
keywordsElasticity
keywordsFoundry coatings
keywordsStress
keywordsShear (Mechanics) AND Stress analysis (Engineering)
treeJournal of Applied Mechanics:;1972:;volume( 039 ):;issue: 002
contenttypeFulltext


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