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Thermal stresses in a multilayer hollow cylinder under thermal shock on its external surface

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

An exact analytical solution of the thermoelasticity problem is presented for a multilayer shallow cylinder with physical properties of the medium that are constant in the limits of each layer. The effect of thermal shock of different intensity as well as the penetration depth of thermal disturbance on the distribution of radial and circumferential thermal stresses has been studied as applied to the one- and two-layer cylinder. It has been shown that the circumferential compressive stresses appear on the external surface of the cylinder under thermal shock while the tensile stresses appear on the internal surface.

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Correspondence to V. A. Kudinov.

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Original Russian Text © V.A. Kudinov, A.V. Eremin, A.E. Kuznetsova, E.V. Stefanyuk, 2014, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2014, No. 1, pp. 30–35.

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Kudinov, V.A., Eremin, A.V., Kuznetsova, A.E. et al. Thermal stresses in a multilayer hollow cylinder under thermal shock on its external surface. Russ. Aeronaut. 57, 37–44 (2014). https://doi.org/10.3103/S1068799814010061

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  • DOI: https://doi.org/10.3103/S1068799814010061

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