L’objectif de cette thèse est de réaliser un système de Contrôle Santé Intégré des structures aéronautiques (CSI ou SHM) autonome et à double-fonctionnalité. Ce système doit être en mesure d’assurer son autonomie énergétique tout en réalisant les tâches de détection et de localisation des endommagements. Latechnique retenue pour alimenter ce système est basée sur la récupération d’énergie vibratoire par transducteurs piézoélectriques SHM collés. Durant ces travaux, un modèle analytique complet de la chaîne de récupération d’énergie vibratoire a d’abord été créé. Ce modèle, validé par la Méthode des ÉlémentsFinis (MEF), permet d’améliorer le rendement du système en déterminant les dimensions, les locali-sations et le type de matériau piézoélectrique idéals des transducteurs. Ce modèle a ensuite été étendu à une configuration plus représentative des conditions de vibrations d’une structure en vol. Une bonne corrélation entre les résultats provenant du modèle prédictif et les essais sur un banc de mesures a étémise en évidence. Une puissance de 1.67mW a été récupérée et la capacité large bande des transducteurs a été vérifiée. L’application de la récupération d’énergie au contrôle de structures composites en cours d’assemblage sur les lignes de production a également été étudiée. Dans ce cas, un transducteur stratégiquement localisé et alimenté par une source de tension disponible génère des ondes de Lambdans la structure afin de pallier l’absence de vibrations naturelles. Un réseau de transducteurs secondaires disséminés sur cette structure récupère et convertit cette énergie vibratoire en énergie électrique. Une puissance de 7.36 mW a été récoltée et ce système a été en mesure de détecter une chute d’outil sur le composite et d’éclairer de façon autonome une diode électroluminescente (DEL) simulant ici la consommation de la transmission sans fil de l’information. / The aim of this thesis is to develop a self-powered Structural Health Monitoring (SHM) system for aeronautical applications. This system has to be fully autonomous and has to be able to carry out SHM tasks such as damage detection and location. The energetic autonomy of the system is provided by a vibrational energy harvesting technology using bonded SHM piezoelectric transducers. In this document,an analytical model of the energy harvesting process has been proposed. This model, validated by the Finite Element Method (FEM), allows the optimization of the energy harvesting system by determining the ideal type of transducers as well as their optimal dimensions and locations. Then, this model has been applied to a configuration aiming to be more representative of the in-flight vibrations experienced by a structure. Good agreement has been found between the analytical simulation and the experimental measurements. A power of 1.67mW has been harvested and the wideband capability of the transducers has been verified. Afterwards, the possibility of using the vibrational energy harvesting technology to control composite structures on assembly line has been investigated. For this case study, a transducer strategically located nearby an available power supply generates Lamb waves throughout the structure to tackle the absence of natural vibration. The remaining sensors, spread all over the structure, convertthe mechanical vibrations into electrical power. Using this technology, a power of 7.36mW has been harvested. Finally, this SHM system has also been able to detect a tool drop on the composite structure and to light simultaneously and autonomously a light-emitting diode (LED) simulating the consumption required to transmit the information wirelessly.

No description available.

The Lamb wave based, non-contact damage detection techniques are developed using the Modified Time Reversal (MTR) method and the model based inverse problem approach. In the first part of this work, the Lamb wave-based MTR method along with the non-contacting sensors is used for structural damage detection. The use of non-contact measurements for MTR method is validated through experimental results and finite element simulations. A novel technique in frequency-time domain is developed to detect linear damages using the MTR method. The technique is highly suitable for the detection of damages in large metallic structures, even when the damage is superficial, and the severity is low. In this technique, no baseline data are used, and all the wave motion measurements are made remotely using a laser vibrometer. Additionally, this novel MTR based technique is not affected due to changes in the material properties of a structure, environmental conditions, or structural loading conditions. Further, the MTR method is improved for two-dimensional damage imaging. The damage imaging technique is successfully tested through experimental results and finite element simulations. In the second part of this work, an inverse problem approach is developed for the detection and estimation of major damage types experienced in adhesive joints. The inverse problem solution is obtained through an optimization algorithm wherein the objective function is formulated using the Lamb wave propagation data. The technique is successfully used for the detection/estimation of cohesive damages, micro-voids, debonds, and weak bonds. Further, the inverse problem solution is separately obtained through a fully connected artificial neural network. The neural network is trained using the Lamb wave propagation data generated from Wavelet Spectral Finite Element (WSFE) model which is computationally much faster than a conventional finite element model. This inverse problem approach technique requires a single point measurement for the inspection of the entire width of the adhesive joint. The proposed technique can be used as an automated quality assurance tool during the manufacturing process, and as an inspection tool during the operational life of adhesively bonded structures.

Résumé : La surveillance de l’intégrité des structures (Structural Health Monitoring - SHM) est une nouvelle technologie, et comme toute nouvelle avancée technologique, elle n’a pas encore réalisé son plein potentiel. Le SHM s’appuie sur des avancées dans plusieurs disciplines, dont l’évaluation non-desctructive, les matériaux intelligents, et les capteurs et actionneurs intégrés. Une des disciplines qui permet son déploiement est la simulation numérique. Le SHM englobe une variété de techniques basées sur la génération d’ondes vibratoires et d’ondes ultrasonores guidées. L’utilisation d’ondes guidées offre en particulier une vaste gamme d’avantages. Le défi majeur associé à la pleine utilisation de la simulation numérique dans la conception d’un système SHM basé sur l’utilisation d’ondes guidées réside dans les ressources de calcul requises pour une simulation précise. La principale raison pour ces exigences est la dispersion induite par la discrétisation numérique, tel qu’indiqué dans la littérature. La méthodes des éléments spectraux (SEM) est une variante de la p-version de la méthode des éléments finis (FEM) qui offre certains outils pour solutionner le problème des erreurs de dispersion, mais la littérature souffre toujours d’une lacune dans l’étude systématique des erreurs de dispersion numérique et de sa dépendance sur les paramètres de simulation. Le présent ouvrage tente de combler cette lacune pour les théories d’ingénierie en vibrations. Il présente d’abord le développement de la formulation des éléments spectraux pour différentes théories d’ingénierie pertinentes pour la propagation des ondes vibratoires dans différents types de structures, comme des tiges et des plaques. Puis, une nouvelle technique pour le calcul des erreurs de dispersion numériques est présentée et appliquée systématiquement dans le but d’évaluer la dispersion numérique induite en termes d’erreurs dans les vitesses de propagation. Cette technique est utilisable pour les différentes formes de propagation des ondes vibratoires dans les éléments structuraux visés dans la présente thèse afin d’évaluer quantitativement les exigences de précision en termes de paramètres de maillage. Les ondes de Lamb constituent un cas particulier de la déformation plane des ondes élastiques, en raison de la présence des doubles frontières à traction libre qui couplent les ondes longitudinales et de cisaillement et qui conduisent à une infinité de modes propagatifs qui sont dispersifs par nature. La simulation des ondes de Lamb n’a pas fait l’objet d’analyse systématique de la dispersion numérique dans la littérature autant pour la SEM que la FEM. Nous rapportons ici pour la première fois les résultats de l’analyse de dispersion numérique pour la propagation des ondes Lamb. Pour toutes les analyses de dispersion numérique présentées ici, l’analyse a été effectuée à˘ala fois dans le domaine fréquentiel et dans le domaine temporel. En se basant sur la nouvelle compréhension des effets de discrétisation numérique de la propagation des ondes guidées, nous étudions l’application de la SEM à la simulation numérique pour des applications de conception en SHM. Pour ce faire, l’excitation piézoélectrique est développée, et une nouvelle technique de condensation statique est développée et mise en œuvre pour les équations de la matrice semi-discrète, qui élimine le besoin de solution itérative, ainsi surnommée fortement couplée ou entièrement couplée. Cet élément piézoélectrique précis est ensuite utilisé pour étudier en détails les subtilités de la conception d’un système SHM en mettant l’accent sur la propagation des ondes de Lamb. Afin d’éviter la contamination des résultats par les réflexions sur les bords une nouvelle forme particulière d’élément absorbant a été développée et mise en œuvre. Les résultats de simulation dans le domaine fréquentiel jettent un éclairage nouveau sur les limites des modèles théoriques actuels pour l’excitation des ondes de Lamb par piézoélectriques. L’excitation par un élément piézoélectrique couplé est ensuite entièrement simulée dans le domaine temporel, et les résultats de simulation sont validés par deux cas de mesures expérimentales ainsi que par la simulation classique avec des éléments finis en utilisant le logiciel commercial ANSYS. // Abstract : Structural health monitoring (SHM) is a novel technology, and like any new technological advancement it has yet not realized its full potential. It builds on advancements in several disciplines including nondestructive evaluation, smart materials, and embedded sensors and actuators. One of the enabling disciplines is the numerical simulation. SHM encompasses a variety of techniques, vibration based, impedance and guided ultrasonic waves. Guided waves offers a wide repertoire of advantages. The major challenge facing the full utilization of the numerical simulation in designing a viable guided waves based SHM System is the formidable computational requirements for accurate simulation. The main reason for these requirements is the dispersion induced by numerical discretization as explained in the literature review. The spectral element (SEM) is a variant of the p-version finite element (FEM) that offers certain remedies to the numerical dispersion errors problem, yet it lacks a systematic study of the numerical dispersion errors and its dependence on the meshing parameters. The present work attempts to fill that gap for engineering theories. It starts by developing the formulation of the spectral element for different relevant engineering theories for guided waves propagation in various structural elements, like rods and plates. Then, extending the utility of a novel technique for computing the numerical dispersion errors, we systematically apply it in order to evaluate the numerically induced dispersion in terms of errors in the propagation speeds. This technique is employed for the various forms of guided waves propagation in structural elements covered in the present thesis in order to quantitatively assess the accuracy requirements in terms of the meshing parameters. The Lamb guided waves constitute a special case of the plane strain elastic waves, that is due to the presence of the double traction free boundaries, couple in the section plane and this coupling leads to an infinitude of propagating modes that are dispersive in nature. Lamb waves simulation have not been a subject of numerical dispersion analysis in the open literature neither for SEM nor FEM for that matter. We report here for the first time the numerical dispersion analysis results for Lamb waves propagation. For all the numerical dispersion analysis presented here, the analysis was done for both the frequency domain and time domain analysis. Based on the established understanding of the numerical discretization effects on the guided waves propagation, we utilize this knowledge to study the application of SEM to SHM simulations. In order to do so the piezoelectric excitation is developed, and a new static condensation technique is developed for the semidiscrete matrix equations, that eliminate the need for iterative solution, thus dubbed strongly coupled or fully coupled implementation. This accurate piezoelectric element are then used to study in details the intricacies of the design of an SHM system with specific emphasis on the Lamb waves propagation. In order to avoid the contamination of the results by the reflections from the edges a new special form of absorbing boundary was developed and implemented. The Simulation results in the frequency domain illuminated the limitations of the current theoretical models for piezoelectric excitation of Lamb waves. The piezoelectric excitation of a fully coupled element is then simulated in the time domain, and the results of simulation was verified against two cases of experimental measurements as well as conventional finite element simulation using the commercial software ANSYS.

Orientador: Jozué Vieira Filho / Resumo: As técnicas de detecção de danos baseadas na Impedância Eletromecânica (EMI) baseiam-se na capacidade dos materiais piezoeléctricos em atuar como sensores e atuadores e contribuem para o desenvolvimento de sistemas de Structural Health Monitoring (SHM). As técnicas clássicas baseadas na EMI utilizam um transdutor Pb-Lead Zirconate Titanite (PZT ) ligado à estrutura monitorada e medem a assinatura de impedância do PZT. No entanto, as técnicas baseadas na EMI dependem de diferentes fatores, como faixa de frequência, número de PZT, temperatura ambiente, tipo de estrutura, entre outros. Assim, para demonstrar a eficácia dos métodos baseados na EMI, faz-se necessário realizar experimentos práticos, o que não é uma tarefa trivial, considerando tais fatores. Portanto, neste trabalho são estudados e propostos procedimentos para criar modelos numéricos, usando elementos finitos (FE), de técnicas baseadas na EMI usando o software PZFlex®. Além disso, os modelos desenvolvidos são usados para propor uma técnica inovadora de compensação de temperatura em sistemas baseados na EMI. Foram modeladas, simuladas e analisadas algumas estruturas clássicas como placa-de-alumínio/PZT e tubo-de-aço/PZT. Os resultados das simulações foram comparados com os equivalentes obtidos com modelos experimentais reais e mostraram-se fortemente correlacionados, indicando que o modelo proposto pode ser uma ferramenta poderosa para o desenvolvimento de técnicas de SHM baseadas na EMI. Foram realizadas simulações ... (Resumo completo, clicar acesso eletrônico abaixo) / Abstract: The damage detection techniques based on the Electromechanical Impedance (EMI) rely on the ability of piezoelectric materials in acting as sensors and actuators and contribute to the development of Structural Health Monitoring (SHM) systems. The classical EMI-based techniques use a Pb-Lead Zirconate Titanite (PZT) transducer bonded to the monitored structure and measure the impedance signature of the PZT. However, the techniques based on EMI depend on different factors, such as frequency range, number of PZTs, environmental temperature, type of structure, among others. Thus, to demonstrate the effectiveness of EMI-based methods, it is necessary to carry out practical experiments, which is not a trivial task considering such factors. Therefore, in this work, it is studied and proposed procedures to create numerical models of techniques based on the EMI, using finite elements (FE) and the PZFlex® software. In addition, the developed models are used to propose an innovative temperature compensation technique for EMI-based systems. Some classical structures were modelled, simulated and analyzed, such as aluminum plate/PZT and steel pipe/PZT. The results of the simulations were compared with the equivalents obtained by experimental models and showed to be strongly correlated, indicating that the proposed model can be a powerful tool for the development of EMI-based SHM techniques. Simulations were performed to analyze the behavior of the signatures under the effect of temperature,... (Complete abstract click electronic access below) / Doutor

Ce travail s’inscrit dans le cadre de la mise en place d’une stratégie de SHM (Structural Health Monitoring) dédiée à la surveillance des structures en génie civil. Il a porté, d’une part, sur l’étude des méthodes de détection et de localisation de l’endommagement du bâti existant et, d’autre part, sur l’élaboration du cahier des charges d’un capteur « intégré » capable de délivrer des informations par transmission compacte des données pour les communiquer à une chaîne SHM. Des études numériques et expérimentales ont été réalisées dans cet objectif. L’état de l’art a clairement mis en évidence plusieurs points faibles des méthodes de détection et de localisation d’endommagements usuelles comme, par exemple, le manque de précision et/ou la complexité de mise en place. On observe aussi que la sensibilité de ces méthodes par rapport à plusieurs paramètres, essentiellement la direction de mesure, le positionnement des capteurs et la sévérité des endommagements, ne permet pas à ce jour de dresser un diagnostic précis de l’état de santé des structures. Pour répondre au cahier des charges d’une chaîne SHM, un Algorithme de Détection et de Localisation (ADL) a été élaboré. Cet algorithme fait appel à des méthodes utilisant les paramètres modaux, essentiellement les fréquences propres et les déformées modales. Leurs mises en œuvre séquentielles et itératives, judicieusement structurées et pilotées,a permis de répondre aux objectifs fixés. Les paramètres modaux requis sont identifiés à l’aide des techniques d’Analyse Modale Opérationnelle (AMO) et à partir de la réponse en accélérations des structures. Deux algorithmes d’AMO ont été utilisés pour leur efficacité et pour leur aptitude à l’automatisation: la méthode stochastique par sous ensemble (SSI), et la méthode de décomposition dans le domaine fréquentiel (FDD). En fusionnant les algorithmes d’AMO avec l’ADL, une chaîne complète de surveillance a été créée. La validation des algorithmes et de la chaîne de surveillance s’est faite à plusieurs niveaux. Tout d’abord, basés sur la théorie des éléments finis, des modèles numériques de la tour de l'Ophite et du pont canadien de la Rivière aux-Mulets ont permis d'évaluer l'ADL. Ces modèles sont endommagés par des signaux sismiques et fournissent les données accélérométriques, données d’entrée du logiciel que nous avons développé. Les résultats obtenus sont tout à fait satisfaisants voire meilleurs que ceux issus des méthodes usuelles. Dans un second temps, nous avons traité des données expérimentales «réelles », issues des mesures accélérométriques sur la tour de l’Ophite. La confrontation entre les résultats d’identification des fréquences propres et des déformées modales issus des algorithmes d’AMO et ceux reportés par la bibliographie, a révélé l’efficacité des algorithmes développés.Enfin, une maquette d’un bâtiment à échelle réduite a également été élaborée et instrumentée.L’application de la chaine de surveillance a permis, d’une part, de détecter et localiser l’endommagement introduit dans la structure et, d’autre part, de mettre en évidence l’intérêt de la surveillance automatique. Finalement, une étude a été menée dans le but de réduire la quantité d’informations enregistrées sur les structures et de faciliter le transfert des données servant comme entrées de la chaîne de surveillance. Les résultats de ces études ont contribué à la spécification d’un nouveau système de surveillance

Commercial composite aerospace structure is required to be designed and managed under the damage tolerant principle. Airworthiness is maintained through a process of regulated inspections and if required maintenance. Currently inspections use visual and assisted visual (non-destructive inspection - NDI) techniques. Damage tolerant operation is therefore reliant on inspectability. Unlike metal structure composite and adhesively bonded structure may show few if any recognisable indicators prior to rapid failure, either visually or using NDI. Although stringent manufacturing processes are demanded to best ensure components are fit for service strategies such as reducing stresses by oversizing components or in the case of bonded features additional mechanical fasteners may be included to allow operation with this potential structural uncertainty. Structural Heath Monitoring (SHM) uses data from in-situ sensors to assess the condition of the structure. If via SHM any uncertainty associated with difficult to inspect components could be eliminated less reliance would be required of additional structure or features allowing lighter and more efficient structure to be viable with no impact on current airworthiness demands. Despite much previous research no SHM system is in use with in-service composite or bonded aerospace components. When operating a structure under Damage-tolerance operational requirements damage must be positively identified to allow repairs to be made whist ensuring appropriate airworthiness demands are maintained. Such demands must also be met by structure inspected using SHM. Unlike previous studies this research combines the process of structural design and in-situ monitoring to address the issues identified. Termed SHM enabled design this approach allows the implementation of monitoring technology and the potential for benefits including the reduced reliance on inefficient additional structure to be viably included in actual structure ... [cont.].

Orientador: Fabrício Guimarães Baptista / Banca: Paulo Sérgio da Silva / Banca: Carlos de Marqui Junior / Resumo: Esta dissertação de mestrado apresenta uma análise experimental da viabilidade do uso dos diafragmas piezelétricos comerciais de baixo custo (comumente conhecidos como buzzers) em sistemas de monitoramento de integridade estrutural (SHM - Structural Health Monitoring) baseados na técnica da impedância eletromecânica (E/M). Esse tipo de aplicação tem recebido uma atenção especial nas últimas décadas por se basear no uso de transdutores piezelétricos pequenos e leves que operam simultaneamente como sensores e atuadores. Foram realizados vários testes em barras de alumínio utilizando diafragmas de diversos tamanhos; as assinaturas de impedância elétrica e os índices de dano foram comparados com os obtidos usando uma cerâmica convencional de PZT (Pb-lead Zirconate Titanate - titanato zirconato de chumbo), que é o transdutor mais comumente utilizado nessa aplicação. Os danos estruturais foram simulados utilizando-se massas metálicas (porcas de parafuso), as quais foram fixadas nas barras com cola a base de cianoacrilato. Quatro tipos de experimentos foram realizados para fins de comparação: estimação da sensibilidade dos transdutores utilizando método da quebra do grafite (PLB - Pencil Lead Break - quebra do grafite); comparação dos índices de dano RMSD (root mean square deviation - desvio da raiz média quadrática) e CCDM (correlation coefficient deviation metric - métrica do desvio do coeficiente de correlação), calculados a partir das assinaturas de impedância; avaliação dos efe... (Resumo completo, clicar acesso eletrônico abaixo) / Abstract: This dissertation presents an experimental analysis of the viability of low-cost commercial piezoelectric diaphragms (commonly known as buzzers) in structural health monitoring (SHM) systems based on the electromechanical impedance (EMI) technique. This application has received special attention in recent decades because it is based on the use of small, lightweight piezoelectric transducers operating as both sensors and actuators. Several tests were carried out on aluminum bars using diaphragms of different sizes; the electrical impedance signatures and damage indices were compared with those obtained using a conventional PZT (Pb-Lead Zirconate Titanate) ceramic, which is the most commonly employed transducer in this application. Structural damage was simulated using metallic bolts (steel nut), which were fixed in the bars using cyanoacrylate glue. Four types of experiments were carried out for comparison between the two transducers: sensitivity estimation using the pencil lead break (PLB) method, analysis of the feasibility to detect structural damage using conventional impedance signatures and damage indices, analysis of temperature effects, and determination of the long-term reproducibility of the results. The results indicated that conventional PZT ceramics and diaphragms with similar size exhibit very close characteristics in relation to reproducibility, sensitivity to damage and temperature effects, which leads to the conclusion that the piezoelectric diaphragms are fea... (Complete abstract click electronic access below) / Mestre

The steel through-truss Traffic Bridge, located in Saskatoon, Saskatchewan is over one hundred years old. The bridge has been subject to ongoing maintenance throughout its service life. However, inspection reports from 2005 and 2006 highlighted the severe deterioration experienced primarily by the steel members immediately above and below the deck surface. These reports prompted the City of Saskatoon (COS) to implement a rehabilitation project that involved the installation of a post-tensioning system to relieve the badly corroded bottom chord members of the axial loads due to the self-weight of the structure, in 2006. Due to the severe deterioration and the structural modifications that the Traffic Bridge has endured, a limited scope structural health monitoring (SHM) system, based on strain measurements, was implemented to reduce some of the uncertainty regarding the active load paths occurring at the deck level. The objectives of the SHM study were to obtain more information regarding the actual load paths and ascertain possible types of structural redundancy, to determine how to best model this type of structure, and to find ways to track ongoing deterioration using instrumentation. The SHM study involved controlled truck loading scenarios to permit measurement of the load paths and provide data to compare the measured results to a finite element (FE) model of the instrumented span. In addition, random loading scenarios were used to capture the vertical dynamic response of the structure in order to further refine the FE model. This study focused on the response of one-half of one interior span. A total of 72 strain gauges were installed. The downstream truss was highly instrumented at ten locations, three members of the upstream truss were instrumented to measure the distribution, and the floor joists in the downstream lane were instrumented to establish possible redundancy paths. Using an FE model in combination with the measured strain data, it was found that redundant load paths only existed at the level of the deck. The bottom chord members experienced non-zero strains once the control vehicle was past the span, possibly indicating some level of redundancy. The members believed to relieve a portion of the bottom chord tensile forces included the car joists, edge joists, and the timber deck. The amount of force transferred from the bottom chord to the deck members was found by FE analysis to be highly related to the lateral stiffness of the floor beams. The FE model was adjusted to match the measured results by modifying various modelling parameters. The most important features of the model were that all deck elements were modelled to be located at the elevation of the bottom chord, that the lateral stiffness of the floor beams was reduced by 50% to best represent the transfer of forces to deck elements, and that the stiffness of bottom chord members was reduced to 80% of their pristine values. In combination with calibrated modification factors applied to the measured values, this FE model is believed to be a useful tool to represent the behaviour of the structure to assist in detecting further damage by modelling the strain differential between members, and components of members.

The steel through-truss Traffic Bridge, located in Saskatoon, Saskatchewan is over one hundred years old. The bridge has been subject to ongoing maintenance throughout its service life. However, inspection reports from 2005 and 2006 highlighted the severe deterioration experienced primarily by the steel members immediately above and below the deck surface. These reports prompted the City of Saskatoon (COS) to implement a rehabilitation project that involved the installation of a post-tensioning system to relieve the badly corroded bottom chord members of the axial loads due to the self-weight of the structure, in 2006. Due to the severe deterioration and the structural modifications that the Traffic Bridge has endured, a limited scope structural health monitoring (SHM) system, based on strain measurements, was implemented to reduce some of the uncertainty regarding the active load paths occurring at the deck level. The objectives of the SHM study were to obtain more information regarding the actual load paths and ascertain possible types of structural redundancy, to determine how to best model this type of structure, and to find ways to track ongoing deterioration using instrumentation. The SHM study involved controlled truck loading scenarios to permit measurement of the load paths and provide data to compare the measured results to a finite element (FE) model of the instrumented span. In addition, random loading scenarios were used to capture the vertical dynamic response of the structure in order to further refine the FE model. This study focused on the response of one-half of one interior span. A total of 72 strain gauges were installed. The downstream truss was highly instrumented at ten locations, three members of the upstream truss were instrumented to measure the distribution, and the floor joists in the downstream lane were instrumented to establish possible redundancy paths. Using an FE model in combination with the measured strain data, it was found that redundant load paths only existed at the level of the deck. The bottom chord members experienced non-zero strains once the control vehicle was past the span, possibly indicating some level of redundancy. The members believed to relieve a portion of the bottom chord tensile forces included the car joists, edge joists, and the timber deck. The amount of force transferred from the bottom chord to the deck members was found by FE analysis to be highly related to the lateral stiffness of the floor beams. The FE model was adjusted to match the measured results by modifying various modelling parameters. The most important features of the model were that all deck elements were modelled to be located at the elevation of the bottom chord, that the lateral stiffness of the floor beams was reduced by 50% to best represent the transfer of forces to deck elements, and that the stiffness of bottom chord members was reduced to 80% of their pristine values. In combination with calibrated modification factors applied to the measured values, this FE model is believed to be a useful tool to represent the behaviour of the structure to assist in detecting further damage by modelling the strain differential between members, and components of members.