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| Teaching Since: | May 2017 |
| Last Sign in: | 409 Weeks Ago, 1 Day Ago |
| Questions Answered: | 66690 |
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MCS,PHD
Argosy University/ Phoniex University/
Nov-2005 - Oct-2011
Professor
Phoniex University
Oct-2001 - Nov-2016
When manufacturing the fuselage of a commuter airplane, aluminum plates are adhesively bonded together with lap joints. Because the elastic deformation for a single plate differs from the deformation for two plates in a lap joint, the maxim um shear stress in the adhesive is twice as high as the average shear stress. The shear strength of the adhesive is 20 M Pa, the tensile strength of the aluminum plates is 95 M Pa, and their thickness is 4.0 mm . Calculate the overlapping length needed to make the adhesive joint twice as strong as the aluminum plate.
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