{"title":"Co-rotational 3D shell element using quaternion algebra to account for large rotations: Static and dynamic applications","authors":"Stéphane Grange, David Bertrand","doi":"10.1016/j.finmec.2025.100315","DOIUrl":null,"url":null,"abstract":"<div><div>This paper presents a new co-rotational shell element based on quaternion algebra as a means of parameterizing large rotations. The co-rotational framework is suitable for beam or shell elements and has been extensively studied in the literature. It is based on a decomposition between rigid body motion and local displacements that generate deformation.</div><div>The advantage of this framework lies in the fact that the internal element defined in the co-rotational frame can be derived from a library of elements (possibly in small or large deformations and even with material nonlinearities).</div><div>The present formulation constitutes an extension of a previous work devoted to a beam finite element using quaternion algebra and applied to shell finite elements. Quaternion algebra is used throughout the kinematic chain, and such parameterization offers an alternative to classical co-rotational formulations. The model is developed within the framework of incremental rotation formulations. Once the decomposition between rigid body motion and local displacements has been performed, the principle of virtual work is introduced to calculate the element response projected onto large displacements and rotations.</div><div>The adopted methodology is then exposed for a three-node triangular shell element. For the sake of simplicity and to demonstrate the capabilities of the co-rotational frame with quaternions, DKT (bending) and OPT (membrane) triangular shell elements with small strains are chosen as the internal element.</div><div>One of the main advantages of using quaternions for parameterization lies in their efficiency for dynamic applications, as they allow for a relative straightforward computation of gyroscopic terms. The numerical simulations show a stable mechanical energy of the systems and a good numerical stability.</div><div>Ten distinct static and dynamic numerical applications are also presented and compared to the literature.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"20 ","pages":"Article 100315"},"PeriodicalIF":3.2000,"publicationDate":"2025-06-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Forces in mechanics","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2666359725000113","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"MATERIALS SCIENCE, MULTIDISCIPLINARY","Score":null,"Total":0}
引用次数: 0
Abstract
This paper presents a new co-rotational shell element based on quaternion algebra as a means of parameterizing large rotations. The co-rotational framework is suitable for beam or shell elements and has been extensively studied in the literature. It is based on a decomposition between rigid body motion and local displacements that generate deformation.
The advantage of this framework lies in the fact that the internal element defined in the co-rotational frame can be derived from a library of elements (possibly in small or large deformations and even with material nonlinearities).
The present formulation constitutes an extension of a previous work devoted to a beam finite element using quaternion algebra and applied to shell finite elements. Quaternion algebra is used throughout the kinematic chain, and such parameterization offers an alternative to classical co-rotational formulations. The model is developed within the framework of incremental rotation formulations. Once the decomposition between rigid body motion and local displacements has been performed, the principle of virtual work is introduced to calculate the element response projected onto large displacements and rotations.
The adopted methodology is then exposed for a three-node triangular shell element. For the sake of simplicity and to demonstrate the capabilities of the co-rotational frame with quaternions, DKT (bending) and OPT (membrane) triangular shell elements with small strains are chosen as the internal element.
One of the main advantages of using quaternions for parameterization lies in their efficiency for dynamic applications, as they allow for a relative straightforward computation of gyroscopic terms. The numerical simulations show a stable mechanical energy of the systems and a good numerical stability.
Ten distinct static and dynamic numerical applications are also presented and compared to the literature.