Development and Investigation of Mathematical Models of Thermoelastic Stresses and Strains in Production of Multilayer Structures of Spherical Shape for Aircraft


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Abstract

The adequate mathematical models are developed that allow investigating the thermoelastic stresses and strains arising in production of multilayer structures of spherical shape for aircraft. The method of finite integral transformations was applied to solve the model tasks stated.

About the authors

I. A. Akimov

Orenburg State Pedagogical University

Author for correspondence.
Email: sau@mail.osu.ru
Russian Federation, ul. Sovetskaya 19, Orenburg, 460014

V. V. Tugov

Aerospace Institute

Email: sau@mail.osu.ru
Russian Federation, Prospekt Pobedy 13, Orenburg, 460018

A. I. Akimov

Orenburg Branch

Email: sau@mail.osu.ru
Russian Federation, ul. Yunykh Lenintsev 20, Orenburg, 460047

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