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Temperature strain of a shallow cylindrical shell under local damage of a protective layer

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

The dynamic and static uncoupled thermoelasticity problems for a thin shallow cylindrical shell under the action of local temperature field is considered. This field appears as a result of mechanical damage of a protective layer region.

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References

  1. Antuf’ev, B.A., Dynamics of a Shallow Shell with the Partly Damaged Protective Coating, Izv.Vuz. Av. Tekhnika, 2002, vol. 45, no. 4, pp. 7–9 [Russian Aeronautics (Engl. Transl.). vol. 45, no. 4, pp. 1–5].

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  2. Grigolyuk, E.I., Podstrigach, Ya.S., and Burak, Ya.I., Optimizatsiya nagreva obolochek i plastin (Optimization of Plate and Shell Heating), Kiev: Naukova Dumka, 1979.

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Original Russian Text © B.A. Antuf’ev, 2008, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2008, No. 1, pp.6–8.

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Antuf’ev, B.A. Temperature strain of a shallow cylindrical shell under local damage of a protective layer. Russ. Aeronaut. 51, 1–4 (2008). https://doi.org/10.3103/S1068799808010017

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  • DOI: https://doi.org/10.3103/S1068799808010017

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