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Title: Acoustic emission detection and prediction of fatigue crack propagation in composite patch repairs using neural networks
Author (s): Okafor, Anthony Chukwujekwu
Singh, Navdeep
Singh, Navrag
Department/Lab Affiliations: Intelligent Systems Center
Mechanical & Aerospace Engineering
Keywords: crack detection
fatigue cracks
maintenance engineering
neural nets
Subject Terms: Acoustic emission testing.
Composite materials.
Polymers.
Issue Date: 2007
Publisher: American Institute of Physics
Citation: Okafor, A C., Navdeep Singh, and Navrag Singh. “Acoustic Emission Detection and Prediction of Fatigue Crack Propagation in Composite Patch Repairs Using Neural Networks." Review of Progress in Quantitative Nondestructive Evaluation” Volume 894, pp. 1532-1539, 2007.
Abstract: An aircraft is subjected to severe structural and aerodynamic loads during its service life. These loads can cause damage or weakening of the structure especially for aging military and civilian aircraft, thereby affecting its load carrying capabilities. Hence composite patch repairs are increasingly used to repair damaged aircraft metallic structures to restore its structural efficiency. This paper presents the results of Acoustic Emission (AE) monitoring of crack propagation in 2024-T3 Clad aluminum panels repaired with adhesively bonded octagonal, single sided boron/epoxy composite patch under tension-tension fatigue loading. Crack propagation gages were used to monitor crack initiation. The identified AE sensor features were used to train neural networks for predicting crack length. The results show that AE events are correlated with crack propagation. AE system was able to detect crack propagation even at high noise condition of 10 Hz loading; that crack propagation signals can be differentiated from matrix cracking signals that take place due to fiber breakage in the composite patch. Three back-propagation cascade feed forward networks were trained to predict crack length based on the number of fatigue cycles, AE event number, and both the Fatigue Cycles and AE events, as inputs respectively. Network using both fatigue cycles and AE event number as inputs to predict crack length gave the best results, followed by Network with fatigue cycles as input, while network with just AE events as input had a greater error.
Type: Article - Conference proceedings
text
In Title: Review of Progress in Quantitative Nondestructive Evaluation
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Publisher URL:
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titleAcoustic emission detection and prediction of fatigue crack propagation in composite patch repairs using neural networks
contributor.authorOkafor, Anthony Chukwujekwu
contributor.authorSingh, Navdeep
contributor.authorSingh, Navrag
contributor.deptlabIntelligent Systems Center
contributor.deptlabMechanical & Aerospace Engineering
subjectcrack detection
subjectfatigue cracks
subjectmaintenance engineering
subjectneural nets
subject.LCSHAcoustic emission testing.
subject.LCSHComposite materials.
subject.LCSHPolymers.
date.issued2007
publisherAmerican Institute of Physics
identifier.citationOkafor, A C., Navdeep Singh, and Navrag Singh. “Acoustic Emission Detection and Prediction of Fatigue Crack Propagation in Composite Patch Repairs Using Neural Networks." Review of Progress in Quantitative Nondestructive Evaluation” Volume 894, pp. 1532-1539, 2007.
identifier.pub.URI
http://dx.doi.org/10.1063/1.2718147
description.abstractAn aircraft is subjected to severe structural and aerodynamic loads during its service life. These loads can cause damage or weakening of the structure especially for aging military and civilian aircraft, thereby affecting its load carrying capabilities. Hence composite patch repairs are increasingly used to repair damaged aircraft metallic structures to restore its structural efficiency. This paper presents the results of Acoustic Emission (AE) monitoring of crack propagation in 2024-T3 Clad aluminum panels repaired with adhesively bonded octagonal, single sided boron/epoxy composite patch under tension-tension fatigue loading. Crack propagation gages were used to monitor crack initiation. The identified AE sensor features were used to train neural networks for predicting crack length. The results show that AE events are correlated with crack propagation. AE system was able to detect crack propagation even at high noise condition of 10 Hz loading; that crack propagation signals can be differentiated from matrix cracking signals that take place due to fiber breakage in the composite patch. Three back-propagation cascade feed forward networks were trained to predict crack length based on the number of fatigue cycles, AE event number, and both the Fatigue Cycles and AE events, as inputs respectively. Network using both fatigue cycles and AE event number as inputs to predict crack length gave the best results, followed by Network with fatigue cycles as input, while network with just AE events as input had a greater error.
typeArticle - Conference proceedings
type.DCMITypetext
type.statusFinal version
rightsThis material is presented to ensure timely dissemination of scholarly and technical work. Copyright and all rights therein are retained by authors or by other copyright holders. All persons copying this information are expected to adhere to the terms and constraints invoked by each author's copyright. In most cases, these works may not be reposted without the explicit permission of the copyright holder.
rightscan upload final version
rights.URI
http://ftp.aip.org/aipdocs/forms/copyrght.pdf
relation.isPartOfReview of Progress in Quantitative Nondestructive Evaluation
date.available2008-10-13T20:25:42Z
identifier.persist.URI
http://scholarsmine.mst.edu/post_prints/AcousticEmissionDetectionAndPredictionOfFatigu_09007dcc8058c4f5.html