Exact transcendental stiffness matrices of general beam-columns embedded in elastic mediums

2021 ◽  
Vol 255 ◽  
pp. 106617
Author(s):  
Sondipon Adhikari
2006 ◽  
Vol 33 (3) ◽  
pp. 278-293 ◽  
Author(s):  
Z Canan Girgin ◽  
Konuralp Girgin

A generalized numerical method is proposed to derive the static and dynamic stiffness matrices and to handle the nodal load vector for static analysis of non-uniform Timoshenko beam–columns under several effects. This method presents a unified approach based on effective utilization of the Mohr method and focuses on the following arbitrarily variable characteristics: geometrical properties, bending and shear deformations, transverse and rotatory inertia of mass, distributed and (or) concentrated axial and (or) transverse loads, and Winkler foundation modulus and shear foundation modulus. A successive iterative algorithm is developed to comprise all these characteristics systematically. The algorithm enables a non-uniform Timoshenko beam–column to be regarded as a substructure. This provides an important advantage to incorporate all the variable characteristics based on the substructure. The buckling load and fundamental natural frequency of a substructure subjected to the cited effects are also assessed. Numerical examples confirm the efficiency of the numerical method.Key words: non-uniform, Timoshenko, substructure, elastic foundation, geometrical nonlinearity, stiffness, stability, free vibration.


2003 ◽  
Vol 81 (14) ◽  
pp. 1425-1448 ◽  
Author(s):  
Moon-Young Kim ◽  
Hee-Taek Yun ◽  
Nam-Il Kim

2004 ◽  
Vol 42 (9) ◽  
pp. 1231-1256 ◽  
Author(s):  
Nam-Il Kim ◽  
Byoung-Ju Lee ◽  
Moon-Young Kim

Author(s):  
R. G. Smith ◽  
J. A. Webster

SynopsisA matrix analysis is derived, using the concept of finite elements, for beam-columns of continuously varying cross-section and “small” initial curvature subject to tangential and normal forces acting at discrete points along the centroidal axis.The relationships between loads applied to the ends of the member and their corresponding deformations are established in the form of stiffness matrices, which are the basis of the Equilibrium Method of Analysis of linear or non-linear elastic plane frames composed of such membeis. In addition, the end loads induced by the tangential and normal forces for various types of boundary conditions are obtained.Finally, it is shown that the buckling load may be calculated by the determination of the lowest eigenvalue of a certain matrix, provided there is no lateial translation of the ends of the member.


Sign in / Sign up

Export Citation Format

Share Document