Experimental validation of flexible multibody dynamics beam formulations

被引:21
作者
Bauchau, Olivier A. [1 ]
Han, Shilei [1 ]
Mikkola, Aki [2 ]
Matikainen, Marko K. [2 ]
Gruber, Peter [3 ]
机构
[1] Univ Michigan Shanghai Jiao Tong Univ Joint Inst, Shanghai 200240, Peoples R China
[2] Lappeenranta Univ Technol, Dept Mech Engn, Lappeenranta 53851, Finland
[3] Austrian Ctr Competence Mech GmbH, A-4040 Linz, Austria
基金
芬兰科学院;
关键词
Flexible Multibody Systems; Finite Element; Experimental Data; ABSOLUTE NODAL COORDINATE; CONSTRAINED MECHANICAL SYSTEMS; ENERGY-CONSISTENT INTEGRATION; NULL SPACE METHOD; ELEMENTS; DEFORMATIONS; ROTATION; SHEAR;
D O I
10.1007/s11044-014-9430-y
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this paper, the accuracies of the geometrically exact beam and absolute nodal coordinate formulations are studied by comparing their predictions against an experimental data set referred to as the "Princeton beam experiment." The experiment deals with a cantilevered beam experiencing coupled flap, lag, and twist deformations. In the absolute nodal coordinate formulation, two different beam elements are used. The first is based on a shear deformable approach in which the element kinematics is described using two nodes. The second is based on a recently proposed approach featuring three nodes. The numerical results for the geometrically exact beam formulation and the recently proposed three-node absolute nodal coordinate formulation agree well with the experimental data. The two-node beam element predictions are similar to those of linear beam theory. This study suggests that a careful and thorough evaluation of beam elements must be carried out to assess their ability to deal with the three-dimensional deformations typically found in flexible multibody systems.
引用
收藏
页码:373 / 389
页数:17
相关论文
共 48 条
[1]   APPLICATION OF DEFORMABLE-BODY MEAN AXIS TO FLEXIBLE MULTIBODY SYSTEM DYNAMICS [J].
AGRAWAL, OP ;
SHABANA, AA .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1986, 56 (02) :217-245
[2]  
[Anonymous], 2006, Nonlinear Composite Beam Theory
[3]  
[Anonymous], 2012, P 2 JOINT INT C MULT
[4]  
Bauchau O, 2009, Structural Analysis: With Applications to Aerospace Structures
[5]  
Bauchau OA, 2011, SOLID MECH APPL, V176, P3, DOI 10.1007/978-94-007-0335-3
[6]   Interpolation of finite rotations in flexible multi-body dynamics simulations [J].
Bauchau, O. A. ;
Epple, A. ;
Heo, S. .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART K-JOURNAL OF MULTI-BODY DYNAMICS, 2008, 222 (04) :353-366
[7]  
Bauchau O.A., 1987, J AM HELICOPTER SOC, V32, P60
[8]   LARGE DISPLACEMENT ANALYSIS OF NATURALLY CURVED AND TWISTED COMPOSITE BEAMS [J].
BAUCHAU, OA ;
HONG, CH .
AIAA JOURNAL, 1987, 25 (11) :1469-1475
[9]   NONLINEAR COMPOSITE BEAM THEORY [J].
BAUCHAU, OA ;
HONG, CH .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1988, 55 (01) :156-163
[10]   Three-Dimensional Beam Theory for Flexible Multibody Dynamics [J].
Bauchau, Olivier A. ;
Han, Shilei .
JOURNAL OF COMPUTATIONAL AND NONLINEAR DYNAMICS, 2014, 9 (04)