NASA NTRS · 19810060051
Stresses in adhesively bonded joints - A closed-form solution
Abstract
The general plane strain problem of adhesively bonded structures consisting of two different, orthotropic adherends is considered, under the assumption that adherend thicknesses are constant and small in relation to the lateral dimensions of the bonded region, so that they may be treated as plates. The problem is reduced to a system of differential equations for the adhesive stresses which is solved in closed form, with a single lap joint and a stiffened plate under various loading conditions being considered as examples. It is found that the plate theory used in the analysis not only predicts the correct trend for adhesive stresses but gives surprisingly accurate results, the solution being obtained by assuming linear stress-strain relations for the adhesive.
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Delale, F., Erdogan, F., Aydinoglu, M. N.. 1981-05-01. Stresses in adhesively bonded joints - A closed-form solution. https://ntrs.nasa.gov/citations/19810060051
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