首页> 外文会议>International Conference on Advances in Engineering Structures, Mechanics amp; Construction; 20060514-17; Waterloo(CA) >ASYMPTOTICALLY-CORRECT STRUCTURAL MODELLING OF THIN-WALLED ANISOTROPIC CLOSED CROSS-SECTION ROTATING SLENDER BEAMS
【24h】

ASYMPTOTICALLY-CORRECT STRUCTURAL MODELLING OF THIN-WALLED ANISOTROPIC CLOSED CROSS-SECTION ROTATING SLENDER BEAMS

机译:薄壁各向异性封闭截面旋转凸台的渐近正确的结构建模

获取原文
获取原文并翻译 | 示例

摘要

An application of a comprehensive and compact methodology to obtain the asymptotically-correct stiffness matrix of anisotropic, thin-walled, closed cross-section, and rotating slender beams is presented. The Variational Asymptotic Method (VAM), which utilizes small geometrical parameters inherent to thin-walled slender beams, is used to obtain the displacement and strain fields, and the cross-sectional stiffness matrix without any ad hoc assumptions. The advantage of this approach is that the asymptotically-correct and populated 4 x 4 cross-sectional stiffness matrix provides all the necessary information about the elastic behavior of the rotating beam, thereby nullifying the need for refined beam theories that incorporate higher order deformation modes, like the Vlasov's mode. The implementation of the theory using MATLAB was validated against the Vartiational Asymptotic Beam Sectional Analysis (VABS) computer software, a two-dimensional finite element program that utilizes a more general approach to the VAM that is applicable to thick/thin-walled anisotropic cross-sections with arbitrary geometry. Sample applications of the theory to rotor blades are presented. The paper concludes with a discussion of how the presented material would be used directly in the dynamic modelling of rotating helicopter blades.
机译:提出了一种综合而紧凑的方法,用于获得各向异性,薄壁,闭合截面和旋转细长梁的渐近校正刚度矩阵。变分渐近方法(VAM)利用薄壁细长梁固有的小几何参数,用于获得位移场和应变场以及横截面刚度矩阵,而无需任何临时假设。这种方法的优势在于,渐近校正且填充的4 x 4横截面刚度矩阵提供了有关旋转梁弹性行为的所有必要信息,从而消除了对包含更高阶变形模式的精细梁理论的需求,就像弗拉索夫的模式一样相对于变分渐近束截面分析(VABS)计算机软件(使用有限元程序,该程序对VAM采用了更通用的方法,适用于厚/薄壁各向异性横断面的二维有限元程序)验证了使用MATLAB进行的理论实施。具有任意几何形状的截面。本文介绍了该理论在转子叶片上的示例应用。本文最后讨论了如何将提出的材料直接用于旋转直升机叶片的动态建模。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号