Simulation of delamination in composites under quasi-static and fatigue loading using cohesive zone models

Es desenvolupa una eina de disseny per l'anàlisi de la tolerància al dany en composites. L'eina pot predir el inici i la propagació de fisures interlaminars. També pot ser utilitzada per avaluar i planificar la necessitat de reparar o reemplaçar components durant la seva vida útil. El model desenvolupat pot ser utilitzat tan per simular càrregues estàtiques com de fatiga. El model proposat és un model de dany termodinàmicament consistent que permet simular la delaminació en composites sota càrregues variables. El model es formula dins el context de la Mecànica del Dany, fent ús dels models de zona cohesiva. Es presenta un metodologia per determinar els paràmetres del model constitutiu que permet utilitzar malles d'elements finits més bastes de les que es poden usar típicament. Finalment, el model és també capaç de simular la delaminació produïda per càrregues de fatiga.

Evaluation of hygrothermal effects on the shear properties of Carall composites

Fiber metal laminates are the frontline materials for aeronautical and space structures. These composites consists of layers of 2024-T3-aluminum alloy and composite prepreg layers. When the composite layer is a carbon fiber prepreg, the fiber metal laminate, named Carall, offers significant improvements over current available materials for aircraft structures. While weight reduction and improved damage tolerance characteristics were the prime drivers to develop this new family of materials, it turns out that they have additional benefits, which become more and more important for today's designers, such as cost reduction and improved safety. The degradation of composites is due to environmental effects mainly on the chemical and/or physical properties of the polymer matrix leading to loss of adhesion of fiber/resin interface. Also, the reduction of fiber strength and stiffness are expected due to environmental degradation. Changes in interface/interphase properties leads to more pronounced changes in shear properties than any other mechanical properties. In this work, the influence of moisture in shear properties of carbon fiber/epoxy composites and Carall have been investigated by using interlaminar shear (ILSS) and Iosipescu tests. It was observed that hygrothermal conditioning reduces the Iosipescu shear strength of CF/E and Carall composites due to the moisture absorption in these materials. (c) 2006 Elsevier B.V. All rights reserved.

A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures

Weight reduction and improved damage tolerance characteristics were the prime drivers to develop new family of materials for the aerospace/ aeronautical industry. Aiming this objective, a new lightweight Fiber/ Metal Laminate (FML) has been developed. The combination of metal and polymer composite laminates can create a synergistic effect on many properties. The mechanical properties of FML shows improvements over the properties of both aluminum alloys and composite materials individually. Due to their excellent properties, FML are being used as fuselage skin structures of the next generation commercial aircrafts. One of the advantages of FML when compared with conventional carbon fiber/epoxy composites is the low moisture absorption. The moisture absorption in FML composites is slower when compared with polymer composites, even under the relatively harsh conditions, due to the barrier of the aluminum outer layers. Due to this favorable atmosphere, recently big companies such as EMBRAER, Aerospatiale, Boing, Airbus, and so one, starting to work with this kind of materials as an alternative to save money and to guarantee the security of their aircrafts.

Estudo de tolerância ao dano no compósito processado via RTM de fibra de carbono NCF/resina epóxi CYCOM 890

Pós-graduação em Engenharia Mecânica - FEG

Spark Plasma Sintering of Si3N4-based Ceramics : Sintering mechanism-Tailoring microstructure-Evaluationg properties

Spark Plasma Sintering (SPS) is a promising rapid consolidation technique that allows a better understanding and manipulating of sintering kinetics and therefore makes it possible to obtain Si3N4-based ceramics with tailored microstructures, consisting of grains with either equiaxed or elongated morphology. The presence of an extra liquid phase is necessary for forming tough interlocking microstructures in Yb/Y-stabilised α-sialon by HP. The liquid is introduced by a new method, namely by increasing the O/N ratio in the general formula RExSi12-(3x+n)Al3x+nOnN16-n while keeping the cation ratios of RE, Si and Al constant. Monophasic α-sialon ceramics with tailored microstructures, consisting of either fine equiaxed or elongated grains, have been obtained by using SPS, whether or not such an extra liquid phase is involved. The three processes, namely densification, phase transformation and grain growth, which usually occur simultaneously during conventional HP consolidation of Si3N4-based ceramics, have been precisely followed and separately investigated in the SPS process. The enhanced densification is attributed to the non-equilibrium nature of the liquid phase formed during heating. The dominating mechanism during densification is the enhanced grain boundary sliding accompanied by diffusion- and/or reaction-controlled processes. The rapid grain growth is ascribed to a dynamic ripening mechanism based on the formation of a liquid phase that is grossly out of equilibrium, which in turn generates an extra chemical driving force for mass transfer. Monophasic α-sialon ceramics with interlocking microstructures exhibit improved damage tolerance. Y/Yb- stabilised monophasic α-sialon ceramics containing approximately 3 vol% liquid with refined interlocking microstructures have excellent thermal-shock resistance, comparable to the best β-sialon ceramics with 20 vol% additional liquid phase prepared by HP. The obtained sialon ceramics with fine-grained microstructure show formidably improved superplasticity in the presence of an electric field. The compressive strain rate reaches the order of 10-2 s-1 at temperatures above 1500oC, that is, two orders of magnitude higher than that has been realised so far by any other conventional approaches. The high deformation rate recorded in this work opens up possibilities for making ceramic components with complex shapes through super-plastic forming.

Valutazione analitica delle aree di delaminazione in materiali compositi avanzati soggetti ad impatti a bassa velocità

In questo lavoro di tesi è stato elaborato un modello analitico al fine di ottenere una stima dell’ampiezza di delaminazione a seguito di impatti a bassa velocità in laminati in composito, in particolare carbon/epoxy. Nel capitolo 2 è descritto il comportamento meccanico di tali laminati (equazioni costitutive della singola lamina, dell’intero laminato e costanti ingegneristiche dell’intero laminato per qualsiasi sistema di riferimento). Nel capitolo 3 viene descritta la filosofia di progettazione damage tolerance per tali materiali sottoposti a low-velocity impact (LVI) e richiamato il concetto di structural health monitoring. In particolare vengono descritti i tipi di difetti per un laminato in composito, vengono classificati gli impatti trasversali e si rivolge particolare attenzione agli impatti a bassa velocità. Nel paragrafo 3.4 sono invece elencate diverse tecniche di ispezione, distruttive e non, con particolare attenzione alla loro applicazione ai laminati in composito. Nel capitolo 4 è riportato lo stato dell’arte per la stima e la predizione dei danni dovuti a LVI nei laminati: vengono mostrate alcune tecniche che permettono di stimare accuratamente l’inizio del danno, la profondità dell’indentazione, la rottura delle fibre di rinforzo e la forza massima di impatto. L’estensione della delaminazione invece, è difficile da stimare a causa dei numerosi fattori che influenzano la risposta agli impatti: spesso vengono utilizzati, per tale stima, modelli numerici piuttosto dispendiosi in termini di tempo e di calcolo computazionale. Nel capitolo 5 viene quindi mostrata una prima formula analitica per il calcolo della delaminazione, risultata però inaffidabile perché tiene conto di un numero decisamente ristretto di fattori che influenzano il comportamento agli LVI. Nel capitolo 6 è mostrato un secondo metodo analitico in grado di calcolare l’ampiezza di delaminazione mediante un continuo aggiornamento della deflessione del laminato. Dal confronto con numerose prove sperimentali, sembra che il modello fornisca risultati vicini al comportamento reale. Il modello è inoltre fortemente sensibile al valore della G_IIc relativa alla resina, alle dimensioni del laminato e alle condizioni di vincolo. É invece poco sensibile alle variazioni delle costanti ingegneristiche e alla sequenza delle lamine che costituiscono il laminato. La differenza tra i risultati sperimentali e i risultati del modello analitico è influenzata da molteplici fattori, tra cui il più significativo sembra essere il valore della rigidezza flessionale, assunto costante dal modello.

Fatigue Crack Propagation in Pressurized metallic Fuselages

On the basis of well-known literature, an analytical tool named LEAF (Linear Elastic Analysis of Fracture) was developed to predict the Damage Tolerance (DT) proprieties of aeronautical stiffened panels. The tool is based on the linear elastic fracture mechanics and the displacement compatibility method. By means of LEAF, an extensive parametric analysis of stiffened panels, representative of typical aeronautical constructions, was performed to provide meaningful design guidelines. The effects of riveted, integral and adhesively bonded stringers on the fatigue crack propagation performances of stiffened panels were investigated, as well as the crack retarder contribution using metallic straps (named doublers) bonded in the middle of the stringers bays. The effect of both perfectly bonded and partially debonded doublers was investigated as well. Adhesively bonded stiffeners showed the best DT properties in comparison with riveted and integral ones. A great reduction of the skin crack growth propagation rate can be achieved with the adoption of additional doublers bonded between the stringers.

Biomass and Stored Carbohydrate Compensation after Above-Ground Biomass Removal in a Perennial Herb: Does Environmental Productivity Play a Role?

Many plant species are able to tolerate severe disturbance leading to removal of a substantial portion of the body by resprouting from intact or fragmented organs. Resprouting enables plants to compensate for biomass loss and complete their life cycles. The degree of disturbance tolerance, and hence the ecological advantage of damage tolerance (in contrast to alternative strategies), has been reported to be affected by environmental productivity. In our study, we examined the influence of soil nutrients (as an indicator of environmental productivity) on biomass and stored carbohydrate compensation after removal of aboveground parts in the perennial resprouter Plantago lanceolata. Specifically, we tested and compared the effects of nutrient availability on biomass and carbon storage in damaged and undamaged individuals. Damaged plants of P. lanceolata compensated neither in terms of biomass nor overall carbon storage. However, whereas in the nutrient-poor environment, root total non-structural carbohydrate concentrations (TNC) were similar for damaged and undamaged plants, in the nutrient-rich environment, damaged plants had remarkably higher TNC than undamaged plants. Based on TNC allocation patterns, we conclude that tolerance to disturbance is promoted in more productive environments, where higher photosynthetic efficiency allows for successful replenishment of carbohydrates. Although plants under nutrient-rich conditions did not compensate in terms of biomass or seed production, they entered winter with higher content of carbohydrates, which might result in better performance in the next growing season. This otherwise overlooked compensation mechanism might be responsible for inconsistent results reported from other studies.

REV7 counteracts DNA double-strand break resection and affects PARP inhibition

Error-free repair of DNA double-strand breaks (DSBs) is achieved by homologous recombination (HR), and BRCA1 is an important factor for this repair pathway. In the absence of BRCA1-mediated HR, the administration of PARP inhibitors induces synthetic lethality of tumour cells of patients with breast or ovarian cancers. Despite the benefit of this tailored therapy, drug resistance can occur by HR restoration. Genetic reversion of BRCA1-inactivating mutations can be the underlying mechanism of drug resistance, but this does not explain resistance in all cases. In particular, little is known about BRCA1-independent restoration of HR. Here we show that loss of REV7 (also known as MAD2L2) in mouse and human cell lines re-establishes CTIP-dependent end resection of DSBs in BRCA1-deficient cells, leading to HR restoration and PARP inhibitor resistance, which is reversed by ATM kinase inhibition. REV7 is recruited to DSBs in a manner dependent on the H2AX-MDC1-RNF8-RNF168-53BP1 chromatin pathway, and seems to block HR and promote end joining in addition to its regulatory role in DNA damage tolerance. Finally, we establish that REV7 blocks DSB resection to promote non-homologous end-joining during immunoglobulin class switch recombination. Our results reveal an unexpected crucial function of REV7 downstream of 53BP1 in coordinating pathological DSB repair pathway choices in BRCA1-deficient cells.

A systematic analysis of INO80 in DNA replication

ATP-dependent chromatin remodeling has been shown to be critical for transcription and DNA repair. However, the involvement of ATP-dependent chromatin remodeling in DNA replication remains poorly defined. Interestingly, we found that the INO80 chromatin-remodeling complex is directly involved in the DNA damage tolerance pathways activated during DNA replication. DNA damage tolerance is important for genomic stability and is controlled by formation of either mono-ubiquitinated or multi-ubiquitinated PCNA, which respectively induce error prone or error-free replication bypass of the lesions. In addition, homologous recombination (HR) mediated by the Rad51 pathway is also involved in the DNA damage tolerance pathways. ^ We found that INO80 is specifically recruited to replication origins during S phase in a genome-wide fashion. In addition, DNA combing analysis shows INO80 is required for the resumption of replication at stalled forks induced by methyl methane-sulfonate (MMS). Mechanistically, we find that INO80 is required for PCNA ubiquitination as well as for Rad51 mediated processing of replication forks after MMS treatment. Furthermore, chromatin immunoprecipitation at specific ARSs indicates INO80 is necessary for Rad18 and Rad51 recruitment to replication forks after MMS treatment. Moreover, 2D gel analysis shows INO80 is necessary to process Rad51 mediated intermediates at impeded replication forks. ^ In conclusion, our findings establish a novel role of a chromatin-remodeling complex in DNA damage tolerance pathways and suggest that chromatin remodeling is fundamentally important to ensure faithful replication of DNA and genome stability in eukaryotes. ^

Estudio de la tolerancia al daño de los materiales y sistemas de pretensado

La mayoría de las estructuras de hormigón pretensadas construidas en los últimos 50 años han demostrado una excelente durabilidad cuando su construcción se realiza atendiendo las recomendaciones de un buen diseño así como una buena ejecución y puesta en obra de la estructura. Este hecho se debe en gran parte al temor que despierta el fenómeno de la corrosión bajo tensión típico de las armaduras de acero de alta resistencia. Menos atención se ha prestado a la susceptibilidad a la corrosión bajo tensión de los anclajes de postensado, posiblemente debido a que se han reportado pocos casos de fallos catastróficos. El concepto de Tolerancia al Daño y la Mecánica de la Fractura en estructuras de Ingeniería Civil ha empezado a incorporarse recientemente en algunas normas de diseño y cálculo de estructuras metálicas, sin embargo, aún está lejos de ser asimilado y empleado habitualmente por los ingenieros en sus cálculos cuando la ocasión lo requiere. Este desconocimiento de los aspectos relacionados con la Tolerancia al Daño genera importantes gastos de mantenimiento y reparación. En este trabajo se ha estudiado la aplicabilidad de los conceptos de la Mecánica de la Fractura a los componentes de los sistemas de postensado empleados en ingeniería civil, empleándolo para analizar la susceptibilidad de las armaduras activas frente a la corrosión bajo tensiones y a la pérdida de capacidad portante de las cabezas de anclajes de postensado debido a la presencia de defectos. Con este objeto se han combinado tanto técnicas experimentales como numéricas. Los defectos superficiales en los alambres de pretensado no se presentan de manera aislada si no que existe una cierta continuidad en la dirección axial así como un elevado número de defectos. Por este motivo se ha optado por un enfoque estadístico, que es más apropiado que el determinístico. El empleo de modelos estadísticos basados en la teoría de valores extremos ha permitido caracterizar el estado superficial en alambres de 5,2 mm de diámetro. Por otro lado la susceptibilidad del alambre frente a la corrosión bajo tensión ha sido evaluada mediante la realización de una campaña de ensayos de acuerdo con la actual normativa que ha permitido caracterizar estadísticamente su comportamiento. A la vista de los resultados ha sido posible evaluar como los parámetros que definen el estado superficial del alambre pueden determinar la durabilidad de la armadura atendiendo a su resistencia frente a la corrosión bajo tensión, evaluada mediante los ensayos que especifica la normativa. En el caso de las cabezas de anclaje de tendones de pretensado, los defectos se presentan de manera aislada y tienen su origen en marcas, arañazos o picaduras de corrosión que pueden producirse durante el proceso de fabricación, transporte, manipulación o puesta en obra. Dada la naturaleza de los defectos, el enfoque determinístico es más apropiado que el estadístico. La evaluación de la importancia de un defecto en un elemento estructural requiere la estimación de la solicitación local que genera el defecto, que permite conocer si el defecto es crítico o si puede llegar a serlo, si es que progresa con el tiempo (por fatiga, corrosión, una combinación de ambas, etc.). En este trabajo los defectos han sido idealizados como grietas, de manera que el análisis quedara del lado de la seguridad. La evaluación de la solicitación local del defecto ha sido calculada mediante el empleo de modelos de elementos finitos de la cabeza de anclaje que simulan las condiciones de trabajo reales de la cabeza de anclaje durante su vida útil. A partir de estos modelos numéricos se ha analizado la influencia en la carga de rotura del anclaje de diversos factores como la geometría del anclaje, las condiciones del apoyo, el material del anclaje, el tamaño del defecto su forma y su posición. Los resultados del análisis numérico han sido contrastados satisfactoriamente mediante la realización de una campaña experimental de modelos a escala de cabezas de anclaje de Polimetil-metacrilato en los que artificialmente se han introducido defectos de diversos tamaños y en distintas posiciones. ABSTRACT Most of the prestressed concrete structures built in the last 50 years have demonstrated an excellent durability when they are constructed in accordance with the rules of good design, detailing and execution. This is particularly true with respect to the feared stress corrosion cracking, which is typical of high strength prestressing steel wires. Less attention, however, has been paid to the stress corrosion cracking susceptibility of anchorages for steel tendons for prestressing concrete, probably due to the low number of reported failure cases. Damage tolerance and fracture mechanics concepts in civil engineering structures have recently started to be incorporated in some design and calculation rules for metallic structures, however it is still far from being assimilated and used by civil engineers in their calculations on a regular basis. This limited knowledge of the damage tolerance basis could lead to significant repair and maintenance costs. This work deals with the applicability of fracture mechanics and damage tolerance concepts to the components of prestressed systems, which are used in civil engineering. Such concepts have been applied to assess the susceptibility of the prestressing steel wires to stress corrosion cracking and the reduction of load bearing capability of anchorage devices due to the presence of defects. For this purpose a combination of experimental work and numerical techniques have been performed. Surface defects in prestressing steel wires are not shown alone, though a certain degree of continuity in the axial direction exist. A significant number of such defects is also observed. Hence a statistical approach was used, which is assumed to be more appropriate than the deterministic approach. The use of statistical methods based in extreme value theories has allowed the characterising of the surface condition of 5.2 mm-diameter wires. On the other hand the stress corrosion cracking susceptibility of the wire has been assessed by means of an experimental testing program in line with the current regulations, which has allowed statistical characterisasion of their performances against stress corrosion cracking. In the light of the test results, it has been possible to evaluate how the surface condition parameters could determine the durability of the active metal armour regarding to its resistance against stress corrosion cracking assessed by means of the current testing regulations. In the case of anchorage devices for steel tendons for prestressing concrete, the damage is presented as point defects originating from dents, scratches or corrosion pits that could be produced during the manufacturing proccess, transport, handling, assembly or use. Due to the nature of these defects, in this case the deterministic approach is more appropriate than the statistical approach. The assessment of the relevancy of defect in a structural component requires the computation of the stress intensity factors, which in turn allow the evaluation of whether the size defect is critical or could become critical with the progress of time (due to fatigue, corrosion or a combination of both effects). In this work the damage is idealised as tiny cracks, a conservative hypothesis. The stress intensity factors have been calculated by means of finite element models of the anchorage representing the real working conditions during its service life. These numeric models were used to assess the impact of some factors on the rupture load of the anchorage, such the anchorage geometry, material, support conditions, defect size, shape and its location. The results from the numerical analysis have been succesfully correlated against the results of the experimental testing program of scaled models of the anchorages in poly-methil methacrylate in which artificial damage in several sizes and locations were introduced.

High temperature nanoindentation behavior of Al/SiC multilayers

Nanoscale Al/SiC composite laminates have unique properties, such as high strength, high toughness, and damage tolerance. In this article, the high-temperature nanoindentation response of Al/SiC nanolaminates is explored from room temperature up to 300_C. Selected nanoindentations were analyzed postmortem using focused ion beam and transmission electron microscopy to ascertain the microstructural changes and the deformation mechanisms operating at high temperature.

Failure analysis of prestressed anchor bars

Three broken steel bars from a sewed crack in a dam are reported. The inspection of the fracture surfaces of the prestressed bars suggests that fractures were triggered by small cracks and by the inherent brittleness of the bars, as fracture toughness was about 40 MPa m1/2. The analysis of the failures shows that the usual design requirements for prestressing bars fail to warn against brittle failures if some damage exists. Some recommendations, based on the concept of damage tolerance, are suggested to avoid similar unfortunate incidents.

Tolerancia al daño de acero inoxidable austeno-ferrítico trefilado con resistencia de acero de pretensar

En este trabajo se determina la tolerancia al daño de un acero inoxidable austeno-ferrítico trefilado hasta obtener resistencia propias del acero de pretensado. Para ello se han realizado ensayos de fractura sobre alambres con secciones transversales debilitadas por fisuras de fatiga propagadas desde la superficie exterior. La medida de la tolerancia al daño adoptada es la curva empírica carga de rotura-profundidad de fisura. Para valorar cuantitativamente los resultados, se utilizan las curvas de dos aceros de pretensar eutectoides, respectivamente fabricados por trefilado y por tratamiento térmico de templado y revenido, así como un modelo elemental de colapso plástico por tracción para alambres fisurados. La microestructura austeno-ferrítico de los alambres inoxidables adquiere una marcada orientación en la dirección de trefilado, que induce una fuerte anisotropía de fractura en los alambres y condiciona su mecanismo macroscópico de colapso a tracción cuando están Asurados. Para observar este mecanismo se ha utilizado la técnica VIC-2D de adquisición y análisis computerizado de imágenes digitales en ensayos mecánicos, aplicándola a ensayos de fractura a tracción realizados con probetas planas de alambre inoxidable trefilado Asuradas transversalmente. Damage tolerance of a high strength cold-drawn ferritic-austenitic stainless steel is assessed by means of tensile fracture tests of cracked wires. A fatigue crack was transversally propagated from the wire surface. The damage tolerance curve of the wires results from the empirical failure load when given as a function of crack depth. As a consequence of cold drawing, the wire microstructure is orientated along its longitudinal axis and anisotropic fracture behavior is found at macrostructural level at the tensile failure of the cracked specimens. An in situ optical technique known as video image correlation VIC-2D was used to get an insight into this failure mechanism by tensile testing transversally fatigue cracked plañe specimens extracted from the cold-drawn wires. Additionally, the experimentally obtained damage tolerance curve of the cold-drawn ferritic-austenitic stainless steel wires is compared with that of the two types of high strength eutectoid wires currently used as prestressing steel for concrete. An elementary plástic collapse model for tensile failure of surface cracked wires is used to assess the damage tolerance curves.

Sensibilidad a las entallas del acero inoxidable dúplex fuertemente trefilado

En el presente trabajo se estudia la sensibilidad a las entallas suaves de alambres de acero inoxidable dúplex fuertemente trefilado. Las entallas consideradas son reducciones de la sección transversal del alambre no simétricas respecto al eje de revolución. Tras constatar experimentalmente que los alambres con este tipo de daño fallan por agotamiento plástico, se ha determinado numéricamente la carga de agotamiento plástico en función de la profundidad de entalla empleando un mode-lo computacional de elementos finitos. Los resultados numéricos indican que la mayor deformabilidad del alambre debida a la entalla actúa en favor de su tolerancia al daño y permite que ésta alcance el límite superior dado por la carga de agotamiento a tracción simple del ligamento resistente.This research deals with the sensitivity to blunt notches of highly cold-drawn wires made of dúplex stainless steel. The analyzed notches are actually reductions of the wire cross section, asymmetrically mechanized with respect to the longitudinal wire axis. Once experimentally verified that the notched wires fail by plástic collapse, the failure load was found as a function of notch depth by means of a finite element model. The numerical results show that the higher compliance of the wires provided by the notch increases their damage tolerance up to the upper bound given by the tensile plástic failure load of the notch ligament.