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Through-thickness stress distribution in the adhesive joint for the multilayer composite material

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

The adhesive joint Goland and Reissner model was generalized for the arbitrary number of the adherend layers. This model was used for the stress state analysis in the layered composite rod with metal edging.

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Correspondence to S. S. Kurennov.

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Original Russian Text © S.S. Kurennov, A.G. Koshevoi, A.G. Polyakov, 2015, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2015, No. 2, pp. 10–15.

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Kurennov, S.S., Koshevoi, A.G. & Polyakov, A.G. Through-thickness stress distribution in the adhesive joint for the multilayer composite material. Russ. Aeronaut. 58, 145–151 (2015). https://doi.org/10.3103/S1068799815020026

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  • DOI: https://doi.org/10.3103/S1068799815020026

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