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contributor authorJoachim L. Grenestedt
contributor authorMikael Danielsson
date accessioned2017-05-09T00:15:06Z
date available2017-05-09T00:15:06Z
date copyrightMarch, 2005
date issued2005
identifier issn0021-8936
identifier otherJAMCAV-26590#276_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131250
description abstractElastic-plastic wrinkling of compression loaded sandwich panels made with layered cores was studied analytically and experimentally. A core with a stiff layer near the sandwich skins can improve various properties, including wrinkling and impact strengths, with only a minor weight penalty. The 2D plane stress and plane strain bifurcation problems were solved analytically, save for a determinantal equation which was solved numerically. Experiments were performed on aluminum skin/foam core sandwich panels with different combinations of stiff and soft core materials. Good correlation between experiments and theory was obtained.
publisherThe American Society of Mechanical Engineers (ASME)
titleElastic-Plastic Wrinkling of Sandwich Panels With Layered Cores
typeJournal Paper
journal volume72
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.1828063
journal fristpage276
journal lastpage281
identifier eissn1528-9036
keywordsStress
keywordsBifurcation
keywordsPlane strain
keywordsEquations
keywordsSkin AND Aluminum
treeJournal of Applied Mechanics:;2005:;volume( 072 ):;issue: 002
contenttypeFulltext


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