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NASA NTRS · 20160006299

Strain-Based Damage Determination Using Finite Element Analysis for Structural Health Management

Abstract

A damage determination method is presented that relies on in-service strain sensor measurements. The method employs a gradient-based optimization procedure combined with the finite element method for solution to the forward problem. It is demonstrated that strains, measured at a limited number of sensors, can be used to accurately determine the location, size, and orientation of damage. Numerical examples are presented to demonstrate the general procedure. This work is motivated by the need to provide structural health management systems with a real-time damage characterization. The damage cases investigated herein are characteristic of point-source damage, which can attain critical size during flight. The procedure described can be used to provide prognosis tools with the current damage configuration.

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BibTeXRIS

Hochhalter, Jacob D., Krishnamurthy, Thiagaraja, Aguilo, Miguel A.. 2016-04-01. Strain-Based Damage Determination Using Finite Element Analysis for Structural Health Management. https://ntrs.nasa.gov/citations/20160006299

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