Bond Modelling of prestressed concrete during the prestressing force release

This paper presents an analytical model for simulating the bond between steel and concrete, in precast prestressed concrete elements, during the prestressing force release. The model establishes a relationship between bond stress, steel and concrete stress and slip in such concrete structures. This relationship allows us to evaluate the bond stress in the transmission zone, where bond stress is not constant, along the whole prestressing force release process. The model is validated with the results of a series of tests and is extended to evaluate the transmission length. This capability has been checked by comparing the transmission length predicted by the model and one measured experimentally in a series of tests.

Bond modelling of prestressed concrete during the prestressing force release

This paper presents an analytical model for simulating the bond between steel and concrete, in precast prestressed concrete elements, during the prestressing force release. The model establishes a relationship between bond stress, steel and concrete stress and slip in such concrete structures. This relationship allows us to evaluate the bond stress in the transmission zone, where bond stress is not constant, along the whole prestressing force release process. The model is validated with the results of a series of tests, considering different steel indentation depths and concrete covers and is extended to evaluate the transmission length. This capability has been checked by comparing the transmission length predicted by the model and one measured experimentally in two series of tests.

Study of bond stress-slip relationship and radial dilation in prestressed concrete

This paper presents two test procedures for evaluating the bond stress–slip and the slip–radial dilation relationships when the prestressing force is transmitted by releasing the steel (wire or strand) in precast prestressed elements. The bond stress–slip relationship is obtained with short length specimens, to guarantee uniform bond stress, for three depths of the wire indentation (shallow, medium and deep). An analytical model for bond stress–slip relationship is proposed and compared with the experimental results. The model is also compared with the experimental results of other researchers. Since numerical models for studying bond-splitting problems in prestressed concrete require experimental data about dilatancy angle (radial dilation), a test procedure is proposed to evaluate these parameters. The obtained values of the radial dilation are compared with the prior estimated by numerical modelling and good agreement is reached

Damage tolerance of cold drawn ferritic-austenitic stainless steels wires for prestressed concrete

Damage tolerance of high strength cold-drawn ferritic–austenitic stainless steel wires is assessed by means of tensile fracture tests of cracked wires. The fatigue crack is 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 behaviour 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 is used to get an insight into this failure mechanism by tensile testing transversally fatigue cracked plane specimens extracted from the cold-drawn wires. Finally, the experimentally obtained damage tolerance curve of the cold-drawn ferritic–austenitic stainless steel wires is compared with that of an elementary plastic collapse model and existing data of two types of high strength eutectoid steel currently used as prestressing steel for concrete.

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.

An analytical model for simulating the bond of prestressed concrete during the prestressed force release

A bond analytical model is proposed in this paper. The model is capable of reproducing the bond stress developed between the steel and concrete, in precast prestressed elements, during the entire process of prestressing force release. The bond stress developed in the transmission zone, where the bond stress is not constant, is also obtained. The steel and concrete stresses as well as the slip between both materials can be also estimated by means of the relation established in the model between these parameters and the bond stress. The model is validated with the results of a series of tests, considering different steel indentation depths and concrete covers and it is extended to evaluate the transmission length. This has been checked by comparing the transmission length predicted by the model and one measured experimentally in two series of tests.

An analytical model for simulating the bond of prestressed concrete during the prestressed force release

A bond analytical model is proposed in this paper. The model is capable of reproducing the bond stress developed between the steel and concrete, in precast prestressed elements, during the entire process of prestressing force release. The bond stress developed in the transmission zone, where the bond stress is not constant, is also obtained. The steel and concrete stresses as well as the slip between both materials can be also estimated by means of the relation established in the model between these parameters and the bond stress. The model is validated with the results of a series of tests, considering different steel indentation depths and concrete covers and it is extended to evaluate the transmission length. This has been checked by comparing the transmission length predicted by the model and one measured experimentally in two series of tests.

Optimization of prestressed concrete bridge decks

In this paper a summary of the methods presently used for optimization of prestressed concrete bridge decks is given. By means of linear optimization the sizes of the prestressing cables with a given fixed geometry are obtained. This simple procedure of linear optimization is also used to obtain the ‘best’ cable profile, by combining a series of feasible cable profiles. The results are compared with the ones obtained by other researchers. A step ahead in the field of optimization of prestressed bridge decks is the simultaneous search of the geometry and size of the prestressing cables. A non-linear programming for optimization is used, namely, ‘the steepest gradient method’. The results obtained are compared with the ones computed previously by means of linear programming techniques. Finally, the general problem of structural optimization is considered. This problem consists in finding the sizes and geometries of the prestressing cables as well as the longitudinal variation of the concrete section.

Fatiga en CFRP: Caracterización y Método Óptico para la Estimación del Daño

El desarrollo de nuevas estructuras aeroespaciales optimizadas, utilizan materiales compuestos, para los componentes críticos y subsistemas, principalmente polímeros reforzados con fibra de carbono (CFRP). Un conocimiento profundo del estado de daño por fatiga de estructuras de CFRP avanzado, es esencial para predecir la vida residual y optimizar los intervalos de inspección estructural, reparaciones y/o sustitución de componentes. Las técnicas actuales se basan principalmente en la medición de cargas estructurales a lo largo de la vida útil de la estructura mediante galgas extensométricas eléctricas. Con esos datos, se estima la vida a fatiga utilizando modelos de acumulación de daño. En la presente tesis, se evalúa la metodología convencional para la estimación de la vida a fatiga de un CFRP aeronáutico. Esta metodología está basada en la regla de acumulación de daño lineal de Palmgren-Miner, y es aplicada para determinar la vida a fatiga de estructuras sometidas a cargas de amplitud variable. Se ha realizado una campaña de ensayos con cargas de amplitud constante para caracterizar un CFRP aeronáutico a fatiga, obteniendo las curvas clásicas S-N, en diferentes relaciones de esfuerzo. Se determinaron los diagramas de vida constante, (CLD), también conocidos como diagramas de Goodman, utilizando redes neuronales artificiales debido a la ausencia de modelos coherentes para materiales compuestos. Se ha caracterizado la degradación de la rigidez debido al daño por fatiga. Se ha ensayado un segundo grupo de probetas con secuencias estandarizadas de cargas de amplitud variable, para obtener la vida a fatiga y la degradación de rigidez en condiciones realistas. Las cargas aplicadas son representativas de misiones de aviones de combate (Falstaff), y de aviones de transporte (Twist). La vida a fatiga de las probetas cicladas con cargas de amplitud variable, se comparó con el índice de daño teórico calculado en base a la regla de acumulación de daño lineal convencional. Los resultados obtenidos muestran predicciones no conservativas. Esta tesis también presenta el estudio y desarrollo, de una nueva técnica de no contacto para evaluar el estado de daño por fatiga de estructuras de CFRP por medio de cambios de los parámetros de rugosidad. La rugosidad superficial se puede medir fácilmente en campo con métodos sin contacto, mediante técnicas ópticas tales como speckle y perfilómetros ópticos. En el presente estudio, se han medido parámetros de rugosidad superficial, y el factor de irregularidad de la superficie, a lo largo de la vida de las probetas cicladas con cargas de amplitud constante y variable, Se ha obtenido una buena tendencia de ajuste al correlacionar la magnitud de la rugosidad y el factor de irregularidad de la superficie con la degradación de la rigidez de las probetas fatigadas. Estos resultados sugieren que los cambios en la rugosidad superficial medida en zonas estratégicas de componentes y estructuras hechas de CFRP, podrían ser indicativas del nivel de daño interno debido a cargas de fatiga. Los resultados también sugieren que el método es independiente del tipo de carga de fatiga que ha causado el daño. Esto último hace que esta técnica de medición sea aplicable como inspección para una amplia gama de estructuras de materiales compuestos, desde tanques presurizados con cargas de amplitud constante, estructuras aeronáuticas como alas y colas de aeronaves cicladas con cargas de amplitud variable, hasta aplicaciones industriales como automoción, entre otros. ABSTRACT New optimized aerospace structures use composite materials, mainly carbon fiber reinforced polymer composite (CFRP), for critical components and subsystems. A strong knowledge of the fatigue state of highly advanced (CFRP) structures is essential to predict the residual life and optimize intervals of structural inspection, repairs, and/or replacements. Current techniques are based mostly on measurement of structural loads throughout the service life by electric strain gauge sensors. These sensors are affected by extreme environmental conditions and by fatigue loads in such a way that the sensors and their systems require exhaustive maintenance throughout system life. In the present thesis, the conventional methodology based on linear damage accumulation rules, applied to determine the fatigue life of structures subjected to variable amplitude loads was evaluated for an aeronautical CFRP. A test program with constant amplitude loads has been performed to obtain the classical S-N curves at different stress ratios. Constant life diagrams, CLDs, where determined by means of Artificial Neural Networks due to the absence of consistent models for composites. The stiffness degradation due to fatigue damage has been characterized for coupons under cyclic tensile loads. A second group of coupons have been tested until failure with a standardized sequence of variable amplitude loads, representative of missions for combat aircraft (Falstaff), and representative of commercial flights (Twist), to obtain the fatigue life and the stiffness degradation under realistic conditions. The fatigue life of the coupons cycled with variable amplitude loads were compared to the theoretical damage index calculated based on the conventional linear damage accumulation rule. The obtained results show non-conservative predictions. This thesis also presents the evaluation of a new non-contact technique to evaluate the fatigue damage state of CFRP structures by means of measuring roughness parameters to evaluate changes in the surface topography. Surface roughness can be measured easily on field with non-contact methods by optical techniques such as speckle and optical perfilometers. In the present study, surface roughness parameters, and the surface irregularity factor, have been measured along the life of the coupons cycled with constant and variable amplitude loads of different magnitude. A good agreement has been obtained when correlating the magnitude of the roughness and the surface irregularity factor with the stiffness degradation. These results suggest that the changes on the surface roughness measured in strategic zones of components and structures made of CFRP, could be indicative of the level of internal damage due to fatigue loads. The results also suggest that the method is independent of the type of fatigue load that have caused the damage. It makes this measurement technique applicable for a wide range of inspections of composite materials structures, from pressurized tanks with constant amplitude loads, to variable amplitude loaded aeronautical structures like wings and empennages, up to automotive and other industrial applications.

Optical sensing of the fatigue damage state of CFRP under realistic aeronautical load sequences

We present an optical sensing methodology to estimate the fatigue damage state of structures made of carbon fiber reinforced polymer (CFRP), by measuring variations on the surface roughness. Variable amplitude loads (VAL), which represent realistic loads during aeronautical missions of fighter aircraft (FALSTAFF) have been applied to coupons until failure. Stiffness degradation and surface roughness variations have been measured during the life of the coupons obtaining a Pearson correlation of 0.75 between both variables. The data were compared with a previous study for Constant Amplitude Load (CAL) obtaining similar results. Conclusions suggest that the surface roughness measured in strategic zones is a useful technique for structural health monitoring of CFRP structures, and that it is independent of the type of load applied. Surface roughness can be measured in the field by optical techniques such as speckle, confocal perfilometers and interferometry, among others.

Análisis teórico-experimental de pilares y vigas de hormigón armado reforzados con fibra de carbono

El presente trabajo se refiere al estudio teórico-experimental del comportamiento de pilares y vigas de hormigón armado reforzados con fibra de carbono o CFRP. El análisis se realiza considerando que los pilares se refuerzan mediante la técnica de adhesión de tejidos de fibra de carbono, generando un efecto de confinamiento. Las vigas se refuerzan mediante la incorporación de barras del mismo material, con refuerzos a cortante. El objetivo es poder comparar el estudio analítico de este tipo de refuerzos con resultados experimentales obtenidos con anterioridad a la realización de este documento, y así poder obtener conclusiones de las posibles diferencias. Hay que señalar que los modelos experimentales no forman parte de este estudio. Los ensayos en pilares fueron realizados en sección cuadrada y circular evaluando la rotura a compresión de las piezas, habiendo sido éstas escaladas con un factor de reducción de 2,3. Los ensayos correspondientes a vigas se realizaron en sección rectangular, centrándose en la evaluación de la rotura a flexión y habiendo sido escaladas igualmente, pero con un factor de reducción de 1:2. El documento se estructura en cuatro capítulos, cuyo contenido se expone de forma concisa a continuación. En el capítulo uno o marco teórico se exponen los principios de comportamiento y tipologías de los pilares y vigas de hormigón armado, las bases teóricas de su refuerzo y confinamiento, así como las diversas técnicas de refuerzo existentes. Se detalla la técnica con FRP, comparando y analizando sus ventajas e inconvenientes. En el capítulo dos se expone el proceso de fabricación, refuerzo y resultados de los modelos experimentales realizados para ambos elementos estructurales. La obtención de los modelos teóricos forma parte del capítulo tres, comparándose con los resultados experimentales en el cuarto capítulo. Finalmente, en el último capítulo se presentan las conclusiones obtenidas al realizar esta comparativa en el refuerzo de vigas y pilares con fibra de carbono. This work refers to the theoretical and experimental study of the behavior of CFRP reinforced concrete columns and beams. The analysis was done considering that the pillars are reinforced by CFRP wrapping technique, resulting in a confinement effect. The beams are reinforced by the addition of bars of the same material, with shear reinforcements. The objective is to compare the analytical study of this type of reinforcement with experimental results obtained prior to the performance of this document, and draw conclusions for any differences. Notice that experimental models are not part of this study. The tests were performed on circular and square section pillars, evaluating compression fracture of the pieces, having been scaled down with a factor of 2.3. The tests were performed on rectangular section beams, focusing on evaluation of the bending fracture and being scaled down equally, but with a factor of 1:2. The document is divided into four chapters, whose content is set out concisely below. The chapter one or theoretical framework sets out the principles of behavior and types of columns and beams of reinforced concrete, the theoretical basis of its reinforcement and confinement, as well as various existing reinforcement techniques. CFRP technique it’s detailed, comparing and analyzing their advantages and disadvantages. Chapter two describes the process of manufacture, reinforcement and results of experimental models made for both structural elements. Chapter three shows the obtaining of the theoretical models, comparing them with the experimental results in the fourth chapter. Finally, the last chapter presents the conclusions to make this comparison in the strengthening of beams and columns with carbon fiber.

Análisis de los modelos de comportamiento de vigas de hormigón armado reforzadas a cortante con polímeros armados con fibras (frp). Validación y calibración experimental

Los polímeros armados con fibras (FRP) se utilizan en refuerzos de estructuras de hormigón debido sobre todo a sus excelentes propiedades mecánicas, su resistencia a la corrosión y a su ligereza que se traduce en facilidad y ahorro en el transporte, puesta en obra y aplicación, la cual se realiza de forma muy rápida, con pocos operarios y utilizando medios auxiliares ligeros, minimizándose las interrupciones del uso de la estructura y las molestias a los usuarios. Las razones presentadas anteriormente, han despertado un gran inter´es por parte de diferentes grupos de investigación a nivel mundial y que actualmente se encuentran desarrollando nuevas técnicas de aplicación y métodos de cálculo. Sin embargo, las investigaciones realizadas hasta la fecha, muestran un procedimiento bien definido y aceptado en lo referente al cálculo a flexión, lo cual no ocurre con el refuerzo a cortante y aunque se ha demostrado que el refuerzo con FRP es un sistema eficaz para incrementar la capacidad ´ultima frente a esfuerzos cortantes, también se pone de manifiesto la necesidad de más estudios experimentales y teóricos para avanzar en el entendimiento de los mecanismos involucrados para este tipo de refuerzo y establecer un procedimiento de diseño apropiado que maximice las excelentes propiedades de este material. Los modelos que explican el comportamiento del refuerzo a cortante de elementos de hormigón armado son complejos y sin transposición directa a fórmulas ingenieriles. Las normas actualmente en vigor, generalmente, establecen empíricamente la capacidad cortante como la suma de las capacidades del hormigón y el refuerzo transversal de acero. Cuando un elemento es reforzado externamente con FRP, los modelos son evidentemente aun más complejos. Las guías y recomendaciones existentes proponen calcular la capacidad del elemento añadiendo la resistencia aportada por el refuerzo externo de FRP a la ya dada por el hormigón y acero transversal. Sin embargo, la idoneidad de este acercamiento es cuestionable puesto que no tiene en cuenta una posible interacción entre refuerzos. Con base en lo anterior se da origen al tema objeto de este trabajo, el cual está orientado al estudio a cortante de elementos de hormigón armado (HA), reforzados externamente con material compuesto de tejido unidireccional de fibra de carbono y resina epoxi. Inicialmente se hace una completa revisión del estado actual del conocimiento de la resistencia a cortante en elementos de hormigón armado con y sin refuerzo externo de FRP, prestando especial atención en los mecanismos actuantes estudiados hasta la fecha. La bibliografía consultada ha sido exhaustiva y actualizada lo que ha permitido el estudio de los modelos propuestos más importantes, tanto para la descripción del fenómeno de adherencia entre hormigón-FRP como de la valoración del aporte al cortante total hecho por el FRP, a través de sendas bases de datos de ensayos de pull-out y de vigas de hormigón armado ensayadas a cortante. Con base en todo lo anterior, se expusieron los mecanismos actuantes en el aporte a cortante hecho por el FRP en elementos de hormigón armado y la forma como las principales guías de cálculo existentes hasta la fecha los abordan. De igual forma se define un modelo de resistencia de esfuerzos para el FRP y se proponen dos modelos para el cálculo de las tensiones o deformaciones efectivas, de los cuales uno esta basado en el modelo de adherencia propuesto por Oller (2005) y el otro en una regresión multivariante para los mecanismos expuestos. Como complemento del estudio de los trabajos encontrados en la literatura, se lleva acabo un programa experimental que, además de aportar más registros a la exigua base de datos existentes, aporte mayor luz a los puntos que se consideran están deficientemente resueltos. Dentro de este programa se realizaron 32 ensayos sobre 16 vigas de 4.5 m de longitud (dos ensayos por viga), reforzadas a cortante con tejido unidireccional de CFRP. Finalmente, estos estudios han permitido proponer modificaciones a las formulaciones existentes en los códigos y guías en vigor. Abstract Its excellent mechanical properties, as well as its corrosion resistance and light weight, which make it easy to apply and inexpensive to ship to the worksite, are the basis of the extended use of fiber reinforced polymer (FRP) as external strengthening for structures. FRP strengthening is a rapid operation calling for only limited labor and lightweight ancillary equipment, all of which minimizes both the interruption of facility usage and user inconvenience. These advantages have aroused considerable interest in civil engineering science and technology and have led to countless applications the world over. Research studies on the shear strength of FRP-strengthened members have been much fewer in number and more controversial than the research on flexural strengthening, for which a more or less standardized and generally accepted procedure has been established. The research conducted and a host of applications around the world have shown that FRP strengthening is an effective technique for raising ultimate shear strength, but it has also revealed a need for further experimental and theoretical research to advance in the understanding of the mechanisms involved and establish suitable design procedures that optimize the excellent properties of this material The models that explain reinforced concrete (RC) shear strength behavior are complex and cannot be directly transposed to engineering formulas. The standards presently in place generally establish shear capacity empirically as the sum of the capacities of the concrete and the passive reinforcement. When members are externally strengthened with FRP, the models are obviously even more complex. The existing guides and recommendations propose calculating capacity by adding the external strength provided by the FRP to the contributions of the concrete and passive reinforcement. The suitability of this approach is questionable, however, because it fails to consider the interaction between passive reinforcement and external strengthening. The subject of this work is based in above, which is focused on externally shear strengthening for reinforced concrete members with unidirectional carbon fiber sheets bonded with epoxy resin. v Initially a thorough literature review on shear of reinforced concrete beams with and without external FRP strengthening was performed, paying special attention to the acting mechanisms studied to date, which allowed the study of the most important models both to describe the bond phenomenon as well as calculating the FRP shear contribution, through separate databases of pull-out tests and shear tests on reinforced concrete beams externally strengthened with FRP. Based on above, they were exposed the acting mechanisms in a FRP shear strengthening on reinforced concrete beams and how guidelines deal the topic. The same way, it is defined a FRP stress strength model and two more models are proposed for calculating the effective stress, one of these is based on the Oller (2005) bond model and another one is the data best fit, taking into account most of the acting mechanisms. To complement the theoretical part we develop an experimental program that, in addition to providing more records to the meager existing database provide greater understanding to the points considered poorly resolved. The test program included 32 tests of 16 beams (2 per beam) of 4.5 m long, shear strengthened with FRP, externally. Finally, modifications to the existing codes and guidelines are proposed.

Stress relaxation losses of prestressing steel wires

Prestressed structures are susceptible to relaxation losses which are of significant importance in structural design. After being manufactured, prestressing wires are coiled to make their storage and transportation easier. The possible deleterious effects of this operation on the stress relaxation behavior of prestressing steel wires are usually neglected, though it has been noticed by manufacturers and contractors that when relaxation tests are carried out after a long-time storage, on occasions relaxation losses are higher than those measured a short time after manufacturing. The influence of coiling on the relaxation losses is checked by means of experimental work and confirmed with a simple analytical model. The results show that some factors like initial residual stresses, excessively long-time storage or storage at high temperatures, can trigger or accentuate this damage. However, it is also shown that if the requirements of standards are fulfilled (minimum coiling diameters) these effects can be neglected.

Comparison of vibration and rolling noise emission of resilient and solid monobloc railway wheels in underground lines

Flat or worn wheels rolling on rough or corrugated tracks can provoke airborne noise and ground-borne vibration, which can be a serious concern for nearby neighbours of urban rail transit lines. Among the various treatments used to reduce vibration and noise, resilient wheels play an important role. In conventional resilient wheels, a slightly prestressed V­shaped rubber ring is mounted between the steel wheel centre and tyre. The elastic layer enhances rolling noise and vibration suppression, as well as impact reduction on the track. In this paper the effectiveness of resilient wheels in underground lines, in comparison to monobloc ones, is assessed. The analysed resilient wheel is able to carry greater loads than standard resilient wheels used for light vehicles. It also presents a greater radial resiliency and a higher axial stiffness than conventional V­wheels. The finite element method was used in this study. A quarter car model was defined, in which the wheelset was modelled as an elastic body. Several simulations were performed in order to assess the vibrational behaviour of elastic wheels, including modal, harmonic and random vibration analysis, the latter allowing the introduction of realistic vertical track irregularities, as well as the influence of the running speed. Due to numerical problems some simplifications were needed. Parametric variations were also performed, in which the sensitivity of the whole system to variations of rubber prestress and Poisson’s ratio of the elastic material was assessed.Results are presented in the frequency domain, showing a better performance of the resilient wheels for frequencies over 200 Hz. This result reveals the ability of the analyzed design to mitigate rolling noise, but not structural vibrations, which are primarily found in the lower frequency range.

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.