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Determining the Residual Stress and Strain in Large Polymer-Composite Airplane Components (Stringer Panels)

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Russian Engineering Research Aims and scope

Abstract

To determine the stress and strain in a T800/X850 polymer-composite stringer panel by finite-element modeling, the following methods are employed: the Cooldown method; and polymer modeling, taking account of the polymerization kinetics. The results obtained by these two methods are significantly different.

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Funding

Financial support was provided by the Russian Ministry of Education and Science (contract 075-15-2020-924, November 16, 2020), within the framework of the program for creating and developing the Supersonic Scientific Center (2020–2022).

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Authors and Affiliations

  1. Moscow Aviation Institute, Moscow, Russia

    D. A. Bondarchuk, M. V. Klesareva, R. R. Gadelev & E. V. Nazarov

Authors
  1. D. A. Bondarchuk
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  2. M. V. Klesareva
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  3. R. R. Gadelev
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  4. E. V. Nazarov
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Corresponding authors

Correspondence to D. A. Bondarchuk or M. V. Klesareva.

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Translated by B. Gilbert

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Bondarchuk, D.A., Klesareva, M.V., Gadelev, R.R. et al. Determining the Residual Stress and Strain in Large Polymer-Composite Airplane Components (Stringer Panels). Russ. Engin. Res. 42, 239–243 (2022). https://doi.org/10.3103/S1068798X22030030

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  • DOI: https://doi.org/10.3103/S1068798X22030030

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