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| 003 | MX-MdCICY | ||
| 005 | 20250625153937.0 | ||
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| 090 | _aB-14195 | ||
| 245 | 1 | 0 | _aGeometrically non-linear thermal stress analysis of an adhesively bonded tubular single lap joint |
| 490 | 0 | _vFinite Elements in Analysis and Design, 39(3), p.155-175, 2003 | |
| 520 | 3 | _aIn this study, the geometrically non-linear thermal stress analysis of an adhesively bonded tubular single lap joint subjected to air9ows having di:erent temperature and velocity outside and inside its inner and outer tubes was carried out using the incremental "nite element method. Since the thermal expansion coe<cients of tubes and adhesive were di:erent the thermal strains arising along the adhesive-tube interfaces resulted in high thermal stresses in the adhesive layer and tubes for di:erent end conditions applied to the ends of its outer and inner tubes. The joint region was considerably deformed, and serious stress concentrations occurred around the adhesive free ends. This e:ect became more evident in cases the tube edges were fully restrained. The peak thermal adhesive and tube stresses occurred at the free ends of the adhesive-tube interfaces. In addition, increasing the overlap length had an e:ect of reducing the peak adhesive and tube stresses, and an optimum overlap length=joint length ratio of 0.2 was determined. | |
| 700 | 1 | 2 | _aKemal Apalak, M. |
| 700 | 1 | 2 | _aGünes, R. |
| 700 | 1 | 2 | _aFidanci, L. |
| 856 | 4 | 0 |
_uhttps://drive.google.com/file/d/1jToaf3rfb-JSedIJ5bJ0YlsAW3TiefOC/view?usp=drivesdk _zPara ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx |
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