导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1999, Vol. 20 ›› Issue (6): 549-552.

• 论文 • Previous Articles     Next Articles

APPLICATION OF NONLINEAR INTERVAL ITERATION METHOD TO POST BUCKLING ANALYSIS OF STRUCTURES

TONG Zong-kai1, LI jie2, WANG Shou-mei1, QIU Zhi-ping1   

  1. 1. Institute of Solid Mechanics,Beijing University of Aeronautics and Astronautics, Beijing 100083, China;2. Department of Foundation,Beijing Institute of Costume, Beijing 100026, China
  • Received:1998-08-03 Revised:1998-10-20 Online:1999-12-25 Published:1999-12-25

Abstract: A non linear interval iteration method is applied to trace the post buckling equilibrium path of structures. Two equilibrium configurations of pre buckling and post buckling near critical loads have been obtained automatically, which avoids stopping of iteration resulting from singularity of stiffness matrixes. Some typical numerical examples show that the method can go through limit points and trace the equilibrium path of post buckling. While dealing with the so called snap back problems, the method is especially effective.

Key words: inter val iter atio n method, post -buckling, no n-linearity

CLC Number: