15.5. Buckling Analysis

The following buckling analysis topics are available:

15.5.1. Assumptions and Restrictions

  1. Valid for structural degrees of freedom (DOFs) only.

  2. The structure fails suddenly, with a horizontal force-deflection curve (see Figure 15.6: Types of Buckling Problems).

  3. The structure has constant stiffness effects.

  4. A static solution with prestress effects included (PSTRES,ON) was run.

Figure 15.6:  Types of Buckling Problems

Types of Buckling Problems

15.5.2. Description of Analysis

This analysis type is for bifurcation buckling using a linearized model of elastic stability. Bifurcation buckling refers to the unbounded growth of a new deformation pattern. A linear structure with a force-deflection curve similar to Figure 15.6: Types of Buckling Problems (a) is well modeled by a linear buckling (ANTYPE,BUCKLE) analysis, whereas a structure with a curve like Figure 15.6: Types of Buckling Problems (b) is not (a large deflection analysis ( NLGEOM,ON) is appropriate, see Large Rotation). The buckling problem is formulated as an eigenvalue problem:

(15–107)

where:

= stiffness matrix
= stress stiffness matrix
= ith eigenvalue (used to multiply the loads which generated [S])
= ith eigenvector of displacements

The eigenproblem is solved as discussed in Eigenvalue and Eigenvector Extraction. The eigenvectors are normalized so that the largest component is 1.0. Thus, the stresses (when output) may only be interpreted as a relative distribution of stresses.

By default, the Block Lanczos and Subspace Iteration methods find buckling modes in the range of negative infinity to positive infinity. If the first eigenvalue closest to the shift point is negative (indicating that the loads applied in a reverse direction will cause buckling), the program should find this eigenvalue.


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