Formulation of Explicit Nonlinear Thermoelastic Terms Using Additive Thermal Strains

A new method of including geometrically nonlinear thermoelastic effects in a total Lagrangian finite element formulation is developed and demonstrated. This method provides explicit formulas for the thermoelastic terms, allows greater insight into the relationship between linear and nonlinear thermoelasticity and provides alternative nonlinear solution methods. The explicit formulation is accomplished through defining a new thermal strain term, called the additive thermal strain. The relative difference between the exact thermoelastic load and commonly used approximations is investigated. It is shown that the geometrically nonlinear thermoelastic formulation reduces to the standard linear thermoelastic formulation with appropriate assumptions.

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Publication Details

Journal
AIAA Journal
Published
2025-03-19
DOI
https://doi.org/10.2514/1.j063512
Primary Topic
Composite Structure Analysis and Optimization
Type
article
Field-Weighted Citation Impact
0.00

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article

Formulation of Explicit Nonlinear Thermoelastic Terms Using Additive Thermal Strains

Joshua D. Deaton, Philip Beran, David J. Neiferd, Ramana V. Grandhi
AIAA Journal
Composite Structure Analysis and Optimization
article

Formulation of Explicit Nonlinear Thermoelastic Terms Using Additive Thermal Strains

Joshua D. Deaton, Philip Beran, David J. Neiferd, Ramana V. Grandhi
article en

Abstract

A new method of including geometrically nonlinear thermoelastic effects in a total Lagrangian finite element formulation is developed and demonstrated. This method provides explicit formulas for the thermoelastic terms, allows greater insight into the relationship between linear and nonlinear thermoelasticity and provides alternative nonlinear solution methods. The explicit formulation is accomplished through defining a new thermal strain term, called the additive thermal strain. The relative difference between the exact thermoelastic load and commonly used approximations is investigated. It is shown that the geometrically nonlinear thermoelastic formulation reduces to the standard linear thermoelastic formulation with appropriate assumptions.

AIAA JournalVol. 63(6)
United States Air Force Research Laboratory (US)
Air Force Research Laboratory
Openalex Percentile: Top 94%
Composite Structure Analysis and Optimization
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