Improving Delamination Modeling via Inverse AnalysisSource: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005::page 04024056-1DOI: 10.1061/JAEEEZ.ASENG-5613Publisher: American Society of Civil Engineers
Abstract: Developing constitutive models that can be used to model composite structural systems subjected to impact loads where modeling damage, failure, and delamination are critical is a challenging task. Often processing experimental data to develop the composite material model and, especially, the delamination model can be tedious, subjective, and error prone. In this paper, procedures for characterizing the behavior of laminated unidirectional composites (UDCs) are explained. First, laboratory tests are conducted to obtain the orthotropic material properties of a commonly used composite, IM7-8552. The obtained data are used in the MAT_213 model in LS-DYNA. Second, fracture-related tests, i.e., double-cantilever beam (DCB) and end-notched flexure (ENF) tests, are conducted to obtain the load-displacement responses. Finally, an inverse analysis approach is used by combining response surface methodology (RSM) and gradient-based numerical optimization to find the optimal values of the traction-separation law (TSL) parameters to build the constitutive model for modeling delamination. The developed cohesive zone element (CZE) model is then validated using the experimental results of a quasi-isotropic tension test. It is shown that the overall process of analyzing the experimental data and building a finite-element model is simpler, and the results from the validation test indicate that the developed methodology can yield accurate predictions.
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contributor author | Ashutosh Maurya | |
contributor author | Mohammed Raihan | |
contributor author | Subramaniam Rajan | |
date accessioned | 2024-12-24T10:15:17Z | |
date available | 2024-12-24T10:15:17Z | |
date copyright | 9/1/2024 12:00:00 AM | |
date issued | 2024 | |
identifier other | JAEEEZ.ASENG-5613.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4298577 | |
description abstract | Developing constitutive models that can be used to model composite structural systems subjected to impact loads where modeling damage, failure, and delamination are critical is a challenging task. Often processing experimental data to develop the composite material model and, especially, the delamination model can be tedious, subjective, and error prone. In this paper, procedures for characterizing the behavior of laminated unidirectional composites (UDCs) are explained. First, laboratory tests are conducted to obtain the orthotropic material properties of a commonly used composite, IM7-8552. The obtained data are used in the MAT_213 model in LS-DYNA. Second, fracture-related tests, i.e., double-cantilever beam (DCB) and end-notched flexure (ENF) tests, are conducted to obtain the load-displacement responses. Finally, an inverse analysis approach is used by combining response surface methodology (RSM) and gradient-based numerical optimization to find the optimal values of the traction-separation law (TSL) parameters to build the constitutive model for modeling delamination. The developed cohesive zone element (CZE) model is then validated using the experimental results of a quasi-isotropic tension test. It is shown that the overall process of analyzing the experimental data and building a finite-element model is simpler, and the results from the validation test indicate that the developed methodology can yield accurate predictions. | |
publisher | American Society of Civil Engineers | |
title | Improving Delamination Modeling via Inverse Analysis | |
type | Journal Article | |
journal volume | 37 | |
journal issue | 5 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/JAEEEZ.ASENG-5613 | |
journal fristpage | 04024056-1 | |
journal lastpage | 04024056-16 | |
page | 16 | |
tree | Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005 | |
contenttype | Fulltext |