Accurate buckling load calculations of a thick orthotropic sandwich panel
Source abstract
Abstract
Abstract This paper is concerned with the buckling of thick sandwich panels with orthotropic elastic face sheets bonded to a linear elastic orthotropic core. When such panels are analyzed for axial load carrying capacity, it is now commonplace to adopt the finite element method to carry out computations. The accuracy of the numerical results will depend not only on roundoff and algorithmic errors, but additionally on the approximations made in computing the incremental (second order) work associated in computing the change of configuration from the unbuckled to the buckled state. Here we show that, particularly for orthotropic thick sandwich structures, large errors can be incurred in computing buckling loads with available commercial software, unless the proper work conjugate measures of stress and strain with their stress-dependent tangential moduli are used in the buckling formulation.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Mechanical Behavior of Composites · Structural Load-Bearing Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (8)
Show source-provided references
1. A correlation study of formulations of incremental deformation and stability of continuous bodies10.1115/1.3408976 ↗
2. 2D elastic analysis of the sandwich panel buckling problem: benchmark solutions and accurate finite element formulations
3. Errors caused by non-work-conjugate stress and strain measures and necessary corrections in finite element programs
4. Baz˘ant · 1991
5. Which formulation allows using a constant shear modulus for small-strain buckling of soft-core sandwich structures10.1115/1.1979516 ↗
6. Stability and finite strain of homogenized structures soft in shear: sandwich or fiber composites, and layered bodies10.1016/j.ijsolstr.2005.03.060 ↗
7. End compression of sandwich columns10.1016/S1359-835X(01)00118-X ↗
8. Wrinkling and compression failure transition in sandwich panels10.1177/1099636204030475 ↗