Fuzzy approach for uncertainty analysis of thin walled composite beams
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 20 January 2012
Abstract
Purpose
The purpose of this paper is to develop an analytical approach to evaluate the influence of material uncertainties on cross‐sectional stiffness properties of thin walled composite beams.
Design/methodology/approach
Fuzzy arithmetic operators are used to modify the thin‐walled beam formulation, which was based on a mixed force and displacement method, and to obtain the uncertainty properties of the beam. The resulting model includes material uncertainties along with the effects of elastic couplings, shell wall thickness, torsion warping and constrained warping. The membership functions of material properties are introduced to model the uncertainties of material properties of composites and are determined based on the stochastic behaviors obtained from experimental studies.
Findings
It is observed from the numerical studies that the fuzzy membership function approach results in reliable representation of uncertainty quantification of thin walled composite beams. The propagation of uncertainties is also demonstrated in the estimation of structural responses of composite beams.
Originality/value
This work demonstrates the use of fuzzy approach to incorporate uncertainties in the responses analytically, in turn improving computational efficiency drastically as compared to the Monte‐Carlo method.
Keywords
Citation
Pawar, P.M., Nam Jung, S. and Ronge, B.P. (2012), "Fuzzy approach for uncertainty analysis of thin walled composite beams", Aircraft Engineering and Aerospace Technology, Vol. 84 No. 1, pp. 13-22. https://doi.org/10.1108/00022661211194942
Publisher
:Emerald Group Publishing Limited
Copyright © 2012, Emerald Group Publishing Limited