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NASA-CR-112237

Adhesive-bonded scarf and stepped-lap joints

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1973

Abstract: Continuum mechanics solutions are derived for the static load-carrying capacity of scarf and stepped-lap adhesive-bonded joints. The analyses account for adhesive plasticity and adherend stiffness imbalance and thermal mismatch. The scarf joint solutions include a simple algebraic formula which serves as a close lower bound, within a small fraction of a per cent of the true answer for most practical geometries and materials. Digital computer programs were developed and, for the stepped-lap joints, the critical adherend and adhesive stresses are computed for each step. The scarf joint solutions exhibit grossly different behavior from that for double-lap joints for long overlaps inasmuch as that the potential bond shear strength continues to increase with indefinitely long overlaps on the scarf joints. The stepped-lap joint solutions exhibit some characteristics of both the scarf and double-lap joints. The stepped-lap computer program handles arbitrary (different) step lengths and thickness and the solutions obtained have clarified potentially weak design details and the remedies. The program has been used effectively to optimize the joint proportions.
URI: http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/204578
Subject: ADHESIVE
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    NASA-CR-112237

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:22:12Z
date available2017-09-04T18:22:12Z
date copyright01/01/1973
date issued1973
identifier otherIANKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/204578
description abstractContinuum mechanics solutions are derived for the static load-carrying capacity of scarf and stepped-lap adhesive-bonded joints. The analyses account for adhesive plasticity and adherend stiffness imbalance and thermal mismatch. The scarf joint solutions include a simple algebraic formula which serves as a close lower bound, within a small fraction of a per cent of the true answer for most practical geometries and materials. Digital computer programs were developed and, for the stepped-lap joints, the critical adherend and adhesive stresses are computed for each step. The scarf joint solutions exhibit grossly different behavior from that for double-lap joints for long overlaps inasmuch as that the potential bond shear strength continues to increase with indefinitely long overlaps on the scarf joints. The stepped-lap joint solutions exhibit some characteristics of both the scarf and double-lap joints. The stepped-lap computer program handles arbitrary (different) step lengths and thickness and the solutions obtained have clarified potentially weak design details and the remedies. The program has been used effectively to optimize the joint proportions.
languageEnglish
titleNASA-CR-112237num
titleAdhesive-bonded scarf and stepped-lap jointsen
typestandard
page115
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1973
contenttypefulltext
subject keywordsADHESIVE
subject keywordsADHESIVES
subject keywordsBONDING
subject keywordsCOMPOSITE
subject keywordsCOMPUTER
subject keywordsCOMPUTERS
subject keywordsCONTINUUM
subject keywordsDIGITAL
subject keywordsJOINTS
subject keywordsLAP
subject keywordsMATERIALS
subject keywordsMECHANICS
subject keywordsPROGRAMS
subject keywordsSCARFING
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DSpace software copyright © 2017-2020  DuraSpace
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