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Local structural nonlinearities identification based on the minimum error linear frequency response function

Hamed Kashani (Aerospace Department, Centre of Excellence in Computational Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran)
A.S. Nobari (Aerospace Department, Centre of Excellence in Computational Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 16 October 2009

313

Abstract

Purpose

The purpose of this paper is to consider the dynamic characteristics identification of local structural nonlinearities.

Design/methodology/approach

Proposed identification method is based on minimum error linear frequency response function (MELF). Two different techniques are developed to extract nonlinear element's dynamic behavior from MELF. The first method, in which no pre‐assumed model is considered for the nonlinearity mechanism behavior, is called “direct identification method.” The second method is “model based identification method.”

Findings

Cubic stiffness dynamic characteristics are identified using the proposed techniques as a case study.

Originality/value

The paper shows that the proposed identification technique is simple and free of any sophisticated measurement hardwares and constraints, which is required by most of the methods proposed so far.

Keywords

Citation

Kashani, H. and Nobari, A.S. (2009), "Local structural nonlinearities identification based on the minimum error linear frequency response function", Aircraft Engineering and Aerospace Technology, Vol. 81 No. 6, pp. 522-528. https://doi.org/10.1108/00022660910997829

Publisher

:

Emerald Group Publishing Limited

Copyright © 2009, Emerald Group Publishing Limited

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