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最少自由度板弯有限元
引用本文:周天孝,刘天时.最少自由度板弯有限元[J].航空学报,1989,10(3):104-112.
作者姓名:周天孝  刘天时
作者单位:航空航天部计算技术研究所 (周天孝),航空航天部计算技术研究所(刘天时)
摘    要: 本文用混合刚度有限元方法构造了解薄板弯曲问题的6自由度三角形和8自由度四边形混合刚度板元。数值算例表明性能良好。

关 键 词:有限元  板弯  最少自由度  
收稿时间:1987-11-04;

The PLATE BENDING FINITE ELEMENTS WITH MINIMUM DEGREES OF FREEDOM
Computing Institute of Chines'''' Aeronautical Establishment Zhou Tianxiao and Liu Tianshi.The PLATE BENDING FINITE ELEMENTS WITH MINIMUM DEGREES OF FREEDOM[J].Acta Aeronautica et Astronautica Sinica,1989,10(3):104-112.
Authors:Computing Institute of Chines' Aeronautical Establishment Zhou Tianxiao and Liu Tianshi
Institution:Computing Institute of Chines' Aeronautical Establishment Zhou Tianxiao and Liu Tianshi
Abstract:Two plate bending elements, a triangular element with 6 degrees of freedom and a quadrilateral element with 8 degrees of freedom, are developed according to Mixed Stiffness Method.A mixed element characteristic shared by these two elements is that piecewise linear polynomial deflection and piecewise constant moment components are indepndently assumed. But, different from the mixed methods, the unknown moment variables can be eliminated at element level and only the deflection variables are solved simultaneously. The rigid-body displacement condition is mathematically proved to be satisfied. It is pointed out that the triangular element and nonconfo-rniing Morley's element stiffness matrices are the same. A detailed numerical evaluation is performed.It may thus be seen that the quadrilateral element gives results of engineering accuracy for a variety of plates under different support and loading conditions even when element geometry is changed from quadrilateral to triangular.
Keywords:finite element  plate bending  minimum degrees of freedom  
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