Search NASASearch

NASA NTRS · 20000050368

Stress Recovery and Error Estimation for Shell Structures

Abstract

The Penalized Discrete Least-Squares (PDLS) stress recovery (smoothing) technique developed for two dimensional linear elliptic problems is adapted here to three-dimensional shell structures. The surfaces are restricted to those which have a 2-D parametric representation, or which can be built-up of such surfaces. The proposed strategy involves mapping the finite element results to the 2-D parametric space which describes the geometry, and smoothing is carried out in the parametric space using the PDLS-based Smoothing Element Analysis (SEA). Numerical results for two well-known shell problems are presented to illustrate the performance of SEA/PDLS for these problems. The recovered stresses are used in the Zienkiewicz-Zhu a posteriori error estimator. The estimated errors are used to demonstrate the performance of SEA-recovered stresses in automated adaptive mesh refinement of shell structures. The numerical results are encouraging. Further testing involving more complex, practical structures is necessary.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Yazdani, A. A., Riggs, H. R., Tessler, A.. 2000-01-01. Stress Recovery and Error Estimation for Shell Structures. https://ntrs.nasa.gov/citations/20000050368

Cite the original work for its findings. Save a collection to share your selection of sources.