航空学报 > 1989, Vol. 10 Issue (7): 331-337

基于一种新的弯曲三角形元素的薄板极限分析方法

沈康智1, 诸德培2   

  1. 1. 飞机结构热强度研究所;2. 西北工业大学
  • 收稿日期:1988-06-01 修回日期:1900-01-01 出版日期:1989-07-25 发布日期:1989-07-25

LIMIT ANALYSIS OF THIN PLATES BASED ON A NEW TRIANGULAR ELEMENT

Shen Kangzhi1, Zhu Depei2   

  1. 1. Aircraft thermal structure strength Research Institute;2. Northwestern Polytechmcal University
  • Received:1988-06-01 Revised:1900-01-01 Online:1989-07-25 Published:1989-07-25

摘要:

本文提出了平面薄板极限分析中的一种新的弯曲三角形元素,简化了元素刚阵的形成,大大降低了结构刚阵阶数。用塑性应变模态思想对平面薄板结构进行了极限分析。本文方法具有物理意义明显、数学形式简洁、元素简单、计算量小、实用性强等优点,在若干算例中均取得了满意的结果。

关键词: 新三角形元素, 薄板, 塑性应变模态, 残余应力模态

Abstract:

This paper presents a new triangular element in the limit analysis of thin plates. The element makes it very easy for us to set up the stiffness matrix which is much smaller than those in other methods. With the principle of the steepest climbing path and plastic strain mode method, the residual stress modes can be formed naturally and the stress field of any structure can be easily described as a unified mathematical rule. Thus, the limit analysis can the reduced to a mathematical programming problem. This method has the following advantages, evident physical meanings, simple form of mathematical programming and less calculation. Some numerical examples have given satisfactory results, and that are useful in practical design.

Key words: new triangular element, thin plate, plastic strain mode, residual stress mode