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Simulating the stress–strain state of a thin plate after a thermal shock

A. V. Sedelnikov

https://orcid.org/0000-0003-2698-1348

Samara National Research University, 34, Moskovskoye Shosse, Samara 443086, Samarskaya Oblast, Russia

E-mail Address: axe_backdraft@inbox.ru

Corresponding author.

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S. V. Glushkov

Samara National Research University, 34, Moskovskoye Shosse, Samara 443086, Samarskaya Oblast, Russia

E-mail Address: glushkov@ssau.ru

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V. V. Serdakova

Amur State University, 21, Ignat’yevskoye Shosse, Blagoveshchensk 675027, Amurskaya Oblast, Russia

E-mail Address: valeriay121@yandex.ru

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M. A. Evtushenko

Samara National Research University, 34, Moskovskoye Shosse, Samara 443086, Samarskaya Oblast, Russia

E-mail Address: sputnik@ssau.ru

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, and

E. S. Khnyryova

Samara National Research University, 34, Moskovskoye Shosse, Samara 443086, Samarskaya Oblast, Russia

E-mail Address: khnyryova@gmail.com

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https://doi.org/10.1142/S1793962322500246Cited by:3 (Source: Crossref)

Abstract

The paper is devoted to simulating the impact of a thermal shock on a thin homogeneous plate in the ANSYS package. The assessment of the stress–strain state is carried out and the dynamics of changes in the temperature field of the plate is determined. The obtained results were compared with the data of other authors and can be used when taking into account the thermal shock of large elastic elements of spacecraft.

Keywords:

References

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