NASA-CR-112235
Adhesive-bonded double-lap joints
Year: 1973
Abstract: Explicit 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
Subject: ADHESIVE
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:12:31Z | |
| date available | 2017-09-04T17:12:31Z | |
| date copyright | 01/01/1973 | |
| date issued | 1973 | |
| identifier other | CANKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/136046 | |
| description abstract | Explicit 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 | |
| language | English | |
| title | NASA-CR-112235 | num |
| title | Adhesive-bonded double-lap joints | en |
| type | standard | |
| page | 105 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1973 | |
| contenttype | fulltext | |
| subject keywords | ADHESIVE | |
| subject keywords | ANALYSIS | |
| subject keywords | BONDING | |
| subject keywords | COMPOSITE | |
| subject keywords | FAILURE | |
| subject keywords | FATIGUE | |
| subject keywords | JOINTS | |
| subject keywords | LAP | |
| subject keywords | MATERIALS | |
| subject keywords | STABILITY | |
| subject keywords | STRESS | |
| subject keywords | STRUCTURAL | |
| subject keywords | TESTS |

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