首页> 外文会议>IMECE2009;ASME international mechanical engineering congress and exposition >ARBITRARY GEOMETRY CELLULAR AUTOMATA FOR ELASTODYNAMICS
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ARBITRARY GEOMETRY CELLULAR AUTOMATA FOR ELASTODYNAMICS

机译:弹性动力学的任意几何元胞自动机

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This study extends a recently-developed [1] cellular automata (CA) elastodynamic modeling approach to arbitrary two-dimensional geometries through development of a rule set appropriate for triangular cells. The approach is fully object-oriented (OO) and exploits OO conventions to produce compact, general, and easily-extended CA classes. Meshes composed of triangular cells allow the elastodynamic response of arbitrary two-dimensional geometries to be computed accurately and efficiently. As in the previous rectangular CA method, each cell represents a state machine which updates in a stepped-manner using a local "bottom-up" rule set and state input from neighboring cells. The approach avoids the need to develop partial differential equations and the complexity therein. Several advantages result from the method's discrete, local and object-oriented nature, including the ability to compute on a massively-parallel basis and to easily add or subtract cells in a multi-resolution manner. The extended approach is used to generate the elastodynamic responses of a variety of general geometries and loading cases (Dirichlet and Neumann), which are compared to previous results and/or comparison results generated using the commercial finite element code, COMSOL. These include harmonic interior plate loading, uniform boundary traction, and ramped boundary displacement. Favorable results are reported in all cases, with the CA approach requiring fewer degrees of freedom to achieve similar accuracy, and considerably less code development.
机译:该研究通过开发适合于三角形电池的规则集,扩展了最近开发的[1]蜂窝自动机(CA)弹性动力学建模方法以任意二维几何形状。该方法是完全面向对象的(OO)并利用OO惯例来生产紧凑,一般和易于扩展的CA类。由三角形单元组成的网格允许准确且有效地计算任意二维几何形状的弹性动力学响应。如在以前的矩形CA方法中,每个单元表示状态机,该状态机使用来自相邻小区的本地“自下而上”规则集和状态输入以阶梯方式更新。该方法避免了需要在其中开发部分微分方程和复杂性。由方法的离散,局部和面向对象的性质具有几个优点,包括在大规模平行的基础上计算和以多分辨率方式轻松添加或减去单元的能力。扩展方法用于生成各种一般几何形状和装载案例(Dirichlet和Neumann)的弹性动力学响应,与使用商业有限元代码COMSOL产生的先前的结果和/或比较结果进行比较。这些包括谐波内板装载,均匀的边界牵引力和斜坡边界位移。所有情况下都报告了有利的结果,CA方法需要更少的自由度来实现类似的准确性,并且相当较少的代码开发。

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