Show simple item record

Adhesive-bonded double-lap joints

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:12:31Z
date available2017-09-04T17:12:31Z
date copyright01/01/1973
date issued1973
identifier otherCANKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/136046
description abstractExplicit analytical solutions are derived for the static load carrying capacity of double-lap adhesive-bonded joints. The analyses extend the elastic solution Volkersen and cover adhesive plasticity, adherend stiffness imbalance and thermal mismatch between the adherends. Both elastic-plastic and bi-elastic adhesive representations lead to the explicit result that the influence of the adhesive on the maximum potential bond strength is defined uniquely by the strain energy in shear per unit area of bond. Failures induced by peel stresses at the ends of the joint are examined. This failure mode is particularly important for composite adherends. The explicit solutions are sufficiently simple to be used for design purposes
languageEnglish
titleNASA-CR-112235num
titleAdhesive-bonded double-lap jointsen
typestandard
page105
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1973
contenttypefulltext
subject keywordsADHESIVE
subject keywordsANALYSIS
subject keywordsBONDING
subject keywordsCOMPOSITE
subject keywordsFAILURE
subject keywordsFATIGUE
subject keywordsJOINTS
subject keywordsLAP
subject keywordsMATERIALS
subject keywordsSTABILITY
subject keywordsSTRESS
subject keywordsSTRUCTURAL
subject keywordsTESTS


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record