首页> 外文期刊>International Journal of Aerospace Sciences >Euler Critical Load of Columns by Using Concept of Topological Similarity
【24h】

Euler Critical Load of Columns by Using Concept of Topological Similarity

机译:拓扑相似性概念的列欧拉临界载荷

获取原文
       

摘要

In the design of aircraft frames buckling of spars, treated as columns, is to be taken into account. A new simplified and easy to use methodology for obtaining Euler critical loads of the columns is presented in this paper. It is based on concept of topological similarity used in the Principle of Quasi Work. This principle connects two topologically similar systems thereby leading to a unique concept of reference column. Critical load of columns with different boundary conditions is obtained by using a priory known equation of deflection of buckled reference column. This methodology is easy to use as critical load of columns are obtained by simple multiplications. It eliminates the use of bending moment expressions as well as solution of differential equations unlike conventional methods. The present methodology is successfully applied to columns with different boundary conditions in this paper.
机译:在飞机框架的设计中,应考虑将梁的屈曲视为支柱。本文提出了一种新的简化且易于使用的方法来获得圆柱的欧拉临界载荷。它基于准工作原理中使用的拓扑相似性概念。该原理将两个拓扑相似的系统连接在一起,从而导致了参考柱的独特概念。通过使用先验已知的弯曲参比柱的挠度方程,可以获得具有不同边界条件的柱的临界载荷。这种方法易于使用,因为通过简单的乘法可以获得列的临界载荷。与传统方法不同,它消除了弯矩表达式的使用以及微分方程的求解。本文的方法成功地应用于具有不同边界条件的柱子。

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