Spectral Formulation for Geometrically Exact Beams: A Motion-Interpolation-Based Approach
This paper proposes a novel spectral formulation for geometrically exact beams based on motion interpolation schemes. Motion interpolation schemes based on matrix, quaternion, and geodesic metrics yields simple expressions for the sectional strains and linearized strain–motion relationships at the m...
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description | This paper proposes a novel spectral formulation for geometrically exact beams based on motion interpolation schemes. Motion interpolation schemes based on matrix, quaternion, and geodesic metrics yields simple expressions for the sectional strains and linearized strain–motion relationships at the mesh nodes. Consequently, the expressions for the nodal forces and tangent stiffness matrices of spectral elements are simplified dramatically. Furthermore, the motion formalism is used to describe the kinematics of the problem, leading to equations of motion that present low-order nonlinearities. Spectral elements based on Gauss–Lobatto and Gauss quadrature rules are investigated. For both cases, the combination of the spectral formulation with the motion formalism leads to geometrically exact beam elements that are much simpler to implement than their counterparts based conventional finite element interpolation schemes using a classical description of kinematics. A global parameterization-free generalized-α scheme is used to integrate the equations in time. Numerical examples demonstrate the accuracy of the proposed formulation. The elements based on Gauss–Lobatto quadrature rules are shown to suffer from axial and shear locking, whereas those based on Gauss rules are locking-free. The convergence rate of (N+1)-node spectral elements based on Gauss quadrature rules is about 2N−0.5 to 2N for all three interpolation schemes. As the number of elements increases, the proposed formulation becomes more accurate than its conventional counterpart. |
doi_str_mv | 10.2514/1.J057489 |
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Motion interpolation schemes based on matrix, quaternion, and geodesic metrics yields simple expressions for the sectional strains and linearized strain–motion relationships at the mesh nodes. Consequently, the expressions for the nodal forces and tangent stiffness matrices of spectral elements are simplified dramatically. Furthermore, the motion formalism is used to describe the kinematics of the problem, leading to equations of motion that present low-order nonlinearities. Spectral elements based on Gauss–Lobatto and Gauss quadrature rules are investigated. For both cases, the combination of the spectral formulation with the motion formalism leads to geometrically exact beam elements that are much simpler to implement than their counterparts based conventional finite element interpolation schemes using a classical description of kinematics. A global parameterization-free generalized-α scheme is used to integrate the equations in time. Numerical examples demonstrate the accuracy of the proposed formulation. The elements based on Gauss–Lobatto quadrature rules are shown to suffer from axial and shear locking, whereas those based on Gauss rules are locking-free. The convergence rate of (N+1)-node spectral elements based on Gauss quadrature rules is about 2N−0.5 to 2N for all three interpolation schemes. As the number of elements increases, the proposed formulation becomes more accurate than its conventional counterpart.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J057489</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Equations of motion ; Formalism ; Interpolation ; Kinematics ; Locking ; Mathematical analysis ; Parameterization ; Quadratures ; Quaternions ; Spectra ; Stiffness matrix</subject><ispartof>AIAA journal, 2019-10, Vol.57 (10), p.4278-4290</ispartof><rights>Copyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at ; employ the eISSN to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a288t-2eb3a101ed33b06ee9592850a996a9038564b1b77e210953137a105bb84d722c3</citedby><cites>FETCH-LOGICAL-a288t-2eb3a101ed33b06ee9592850a996a9038564b1b77e210953137a105bb84d722c3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Han, Shilei</creatorcontrib><creatorcontrib>Bauchau, Olivier A</creatorcontrib><title>Spectral Formulation for Geometrically Exact Beams: A Motion-Interpolation-Based Approach</title><title>AIAA journal</title><description>This paper proposes a novel spectral formulation for geometrically exact beams based on motion interpolation schemes. Motion interpolation schemes based on matrix, quaternion, and geodesic metrics yields simple expressions for the sectional strains and linearized strain–motion relationships at the mesh nodes. Consequently, the expressions for the nodal forces and tangent stiffness matrices of spectral elements are simplified dramatically. Furthermore, the motion formalism is used to describe the kinematics of the problem, leading to equations of motion that present low-order nonlinearities. Spectral elements based on Gauss–Lobatto and Gauss quadrature rules are investigated. For both cases, the combination of the spectral formulation with the motion formalism leads to geometrically exact beam elements that are much simpler to implement than their counterparts based conventional finite element interpolation schemes using a classical description of kinematics. A global parameterization-free generalized-α scheme is used to integrate the equations in time. Numerical examples demonstrate the accuracy of the proposed formulation. The elements based on Gauss–Lobatto quadrature rules are shown to suffer from axial and shear locking, whereas those based on Gauss rules are locking-free. The convergence rate of (N+1)-node spectral elements based on Gauss quadrature rules is about 2N−0.5 to 2N for all three interpolation schemes. As the number of elements increases, the proposed formulation becomes more accurate than its conventional counterpart.</description><subject>Equations of motion</subject><subject>Formalism</subject><subject>Interpolation</subject><subject>Kinematics</subject><subject>Locking</subject><subject>Mathematical analysis</subject><subject>Parameterization</subject><subject>Quadratures</subject><subject>Quaternions</subject><subject>Spectra</subject><subject>Stiffness matrix</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNpl0FFLwzAQB_AgCs7pg98gIAg-ZOaSpk1928Y2JxMfVNCncu0y7GiXmrTgvr0ZHfjg03Hwu_8dR8g18JFQEN3D6ImrJNLpCRmAkpJJrT5OyYBzDgwiJc7Jhffb0IlEw4B8vjamaB1WdG5d3VXYlnZHN9bRhbG1aV1ZYFXt6ewHi5ZODNb-gY7psz04tty1xjW2n2IT9GZNx03jLBZfl-Rsg5U3V8c6JO_z2dv0ka1eFsvpeMVQaN0yYXKJwMGspcx5bEyqUqEVxzSNMeXh_DjKIU8SI4CnSoJMAld5rqN1IkQhh-Smzw1rvzvj22xrO7cLKzMheax0DEIHdderwlnvndlkjStrdPsMeHb4XAbZ8XPB3vYWS8S_tP_wF3Amaos</recordid><startdate>20191001</startdate><enddate>20191001</enddate><creator>Han, Shilei</creator><creator>Bauchau, Olivier A</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20191001</creationdate><title>Spectral Formulation for Geometrically Exact Beams: A Motion-Interpolation-Based Approach</title><author>Han, Shilei ; Bauchau, Olivier A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a288t-2eb3a101ed33b06ee9592850a996a9038564b1b77e210953137a105bb84d722c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Equations of motion</topic><topic>Formalism</topic><topic>Interpolation</topic><topic>Kinematics</topic><topic>Locking</topic><topic>Mathematical analysis</topic><topic>Parameterization</topic><topic>Quadratures</topic><topic>Quaternions</topic><topic>Spectra</topic><topic>Stiffness matrix</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Han, Shilei</creatorcontrib><creatorcontrib>Bauchau, Olivier A</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Han, Shilei</au><au>Bauchau, Olivier A</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Spectral Formulation for Geometrically Exact Beams: A Motion-Interpolation-Based Approach</atitle><jtitle>AIAA journal</jtitle><date>2019-10-01</date><risdate>2019</risdate><volume>57</volume><issue>10</issue><spage>4278</spage><epage>4290</epage><pages>4278-4290</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>This paper proposes a novel spectral formulation for geometrically exact beams based on motion interpolation schemes. Motion interpolation schemes based on matrix, quaternion, and geodesic metrics yields simple expressions for the sectional strains and linearized strain–motion relationships at the mesh nodes. Consequently, the expressions for the nodal forces and tangent stiffness matrices of spectral elements are simplified dramatically. Furthermore, the motion formalism is used to describe the kinematics of the problem, leading to equations of motion that present low-order nonlinearities. Spectral elements based on Gauss–Lobatto and Gauss quadrature rules are investigated. For both cases, the combination of the spectral formulation with the motion formalism leads to geometrically exact beam elements that are much simpler to implement than their counterparts based conventional finite element interpolation schemes using a classical description of kinematics. A global parameterization-free generalized-α scheme is used to integrate the equations in time. Numerical examples demonstrate the accuracy of the proposed formulation. The elements based on Gauss–Lobatto quadrature rules are shown to suffer from axial and shear locking, whereas those based on Gauss rules are locking-free. The convergence rate of (N+1)-node spectral elements based on Gauss quadrature rules is about 2N−0.5 to 2N for all three interpolation schemes. As the number of elements increases, the proposed formulation becomes more accurate than its conventional counterpart.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J057489</doi><tpages>13</tpages></addata></record> |
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subjects | Equations of motion Formalism Interpolation Kinematics Locking Mathematical analysis Parameterization Quadratures Quaternions Spectra Stiffness matrix |
title | Spectral Formulation for Geometrically Exact Beams: A Motion-Interpolation-Based Approach |
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