The research effort in this thesis is devoted to develop techniques to accurately and rapidly identify the location, orientation, and magnitude of the defects by using structural health monitoring concepts that use Laser Doppler Vibrometer as a non-contact sensor with multi-point sensing capability. The first research area addresses the formulation and validation of an innovative Damage Measure that is based on the ratios of the strain energy distributions of the damaged and undamaged structure. The innovations include use of a single set of actuator/sensor pair to excite and detect the responses of a structure for low frequency vibrations as well as guided wave propagation studies. A second new capability is the estimation of the Damage Measure without requiring any knowledge of the undamaged baseline structure. This method is made possible because of the development of these new technologies: Spatial Decimation and Wavenumber/Frequency filtering. The third contribution is to develop analytical models for the structural dynamics of damaged structure and seek solutions that use perturbation methods to detect damage in a plate structure. The fourth contribution is the development of a comprehensive damage detection technique over a wide frequency dynamic range. The fifth topic of research involves automation in Structural Health Monitoring based on the comprehensive Damage Measure formulation. Under the control of software the Scanning Laser Doppler Vibrometer is used to acquire the low frequency vibration mode data for a coarse identification of all the suspect regions of damage using a threshold criterion on the Damage Measure. Each suspect region of damage is further investigated using the high frequency elastic wave propagation to clearly identify the location, orientation, and extent of the damage. The computer control of the Laser Doppler Vibrometer and a quantitative assessment of the damage provide the enabling technologies for the automation proof of concept. Finally the developed techniques of damage detection are successfully demonstrated on practical structures such as a turbine blade in the laboratory and an F-15 vertical tail in field maintenance conditions

This thesis presents fundamental research in the field of laser vibrometry for the application to vibration measurements. A key concern for laser vibrometry is the effect of laser speckle which appears when a coherent laser beam scatters from an optically rough surface. The laser vibrometer is sensitive to changes in laser speckle which result from surface motions not in the direction of the incident beam. This adds speckle noise to the vibrometer output which can be indistinguishable from the genuine surface vibrations. This has been termed ‘pseudo-vibration' and requires careful data interpretation by the vibration engineer. This research has discovered that measurements from smooth surfaces, even when no identifiable speckle pattern is generated, can produce noise and therefore reference to speckle noise, in such circumstances, is inappropriate. This thesis has, therefore, adopted the more general term of pseudo-vibration to include noise generated from any surface roughness or treatment, i.e. including but not limited to speckle noise. This thesis develops and implements novel experimental methods to quantify pseudovibration sensitivities (transverse, tilt and rotation sensitivity) with attention focussed on commercially available laser vibrometers and consideration is given to a range of surface roughnesses and treatments. It investigates, experimentally, the fundamental behaviour of speckles and attempts to formulate, for the first time, a relationship between changes in intensity to pseudo-vibration sensitivity levels. The thesis also develops and implements models for computational simulation of pseudo-vibrations using the fundamental behaviour of speckles. The combination of experimentation and simulation improves current understanding of the pseudo-vibration mechanisms and provides the vibration engineer with a valuable resource to improve data interpretation. Two experimental methods of quantifying pseudo-vibration sensitivity are developed and successfully applied in the evaluation of transverse, tilt and rotation sensitivity for two models of commercial laser vibrometer. These evaluations cover both single beam (translational vibration measurement) and parallel beam (for angular vibration measurement) modes. The first method presented requires correction of the vibrometer measurement with an independent measurement of genuine velocity to produce an iii apparent velocity dominated by the required noise components. The second method requires a differential measurement using two vibrometers to cancel common components such as genuine velocity, leaving only uncorrelated noise from each measurement in the resulting apparent velocity. In each case, a third measurement is required of the surface motion component causing pseudo-vibration and this is used to normalise the apparent velocity. Pseudo-vibration sensitivity is then presented as a map showing the spectral shape of the noise, as a mean and standard deviation of harmonic peaks in the map and as a total rms level across a defined bandwidth. The simulations employ a novel and effective approach to modelling speckle evolution. Transverse and tilt sensitivity are predicted for the first time and are verified by the experimental study. They provide the vibration engineer with the potential to estimate pseudo-vibrations using a simple piece of software. The laser beam spot diameter has a large influence on the pseudo-vibration sensitivity. Transverse sensitivity has been quantified as around 0.03% and 0.01% (per order) of the transverse velocity of the surface for beam spot diameters of 100 μm and 600 μm respectively. Larger beam spots have been shown to significantly reduce transverse sensitivity and measurements from smoother surfaces have also shown a reduced level of transverse sensitivity. Tilt sensitivity has been quantified at about 0.1 μms-1/degs-1 and 0.3 μms-1/degs-1 (per order) of angular velocity of the surface for beam spot diameters of 100 μm and 600 μm respectively. Smaller beam spot diameters significantly reduce tilt sensitivity. The surface roughness or treatment has been shown to have little effect on the level of tilt sensitivity. Rotation sensitivity has been quantified at approximately 0.6 μms- 1/rads-1 and 1.9μms-1/rads-1 (per order) of rotation velocity of the rotor for 90 μm and 520 μm. Smaller beam spot diameters have shown a significant reduction in rotation sensitivity and measurements on smoother surfaces have shown a reduced rotation sensitivity. Focussing the laser beam approximately on the rotation axis has also shown a significant reduction in rotation sensitivity. Parallel beam rotation sensitivity has been quantified at 0.016 degs-1/rads-1 and it is demonstrated that this can adequately be estimated using the single beam rotation sensitivity.

In der vorliegenden Arbeit wird eine Methode zur Charakterisierung von Mikrosystemen mit beweglichen Komponenten dargestellt. Sie erlaubt, funktionsrelevante Parameter und deren Schwankungen produktionsbegleitend auf Waferlevel zu ermitteln. Dabei wird vorausgesetzt, dass die Sollform der Struktur und die Abweichungsarten bekannt sind. Die Methode beruht auf dem Vergleich von numerisch berechneten mit experimentell ermittelten Eigenfrequenzen der untersuchten Mikrosysteme. Dazu wird die Abhängigkeit verschiedener Eigenfrequenzen von den gesuchten Parametern mittels einer Parametervariationsanalyse berechnet und durch eine geeignete Funktion angenähert. Die Messung der dynamischen Eigenschaften erfolgt mit Hilfe eines Bewegungsanalysators, der auf einem Laser-Doppler-Vibrometer basiert. Im letzen Schritt werden die gesuchten Parameter berechnet. Kernpunkt der entwickelten Methode sind Messungen auf der Basis von speziellen Teststrukturen, die im Waferlayout neben den eigentlichen Nutzstrukturen platziert sind und parallel mit den Nutzstrukturen prozessiert werden. Es werden Algorithmen zur Generierung des Designs der Teststrukturen und ihrer Platzierung im Waferlayout entwickelt. Dabei werden das Design der Nutzstruktur und deren funktionsrelevante Parameter, der technologische Ablauf und materialspezifische Kennwerte berücksichtigt. Im Ergebnis liegt eine Bibliothek von Standard-Teststrukturen vor, die für produktionsbegleitende Messungen sowie für die Übertragbarkeit der Ergebnisse geeignet sind. Außerdem werden allgemeingültige Richtlinien zur Durchführung der Messungen an den Standard-Teststrukturen abgeleitet. Das Messverfahren wurde an unterschiedlichen Mikrosystemen mit beweglichen Komponenten überprüft und zu einer allgemeinen Messmethode für diese Klasse von Mikrosystemen erweitert. / In this work a method for the characterization of microsystems with movable components is presented. The method allows to determine the relevant parameters and their variations on wafer level if the nominal shape of the structure and the type of deviations are known. The method is based on a comparison of the numerically calculated and experimentally measured Eigenfrequencies of the microsystems. For that purpose, the relationships between various Eigenfrequencies and the searched parameters are calculated by parameter variation analysis and the results of this analysis are approximated with appropriate functions. A Laser Doppler vibrometer based motion analyzer is used to determine the frequency response function of the micromechanical structure and extract Eigenfrequencies. The comparison of the measured and the calculated frequencies provides values for the searched parameters. The key element of the developed method is the measurement on special test structures that are placed in the wafer layout next to the actual microsystems and processed in the same technological process parallel to the actual microsystems. Algorithms for designing the test structures and their placement in the wafer layout are shown, taking into account the design of the actual microsystems and the function parameters of the technological process as well as material characteristics. As a result, a library of standard test structures for function relevant parameters is available. A general guideline for the measurement on the test structures is presented. The presented method is verified on various microsystems and extended to a whole class of microsystems with movable components.

The on-line condition monitoring of turbomachinery blades is of utmost importance to ensure the long term health and availability of such machines and as such has been an area of study since the late 1960s. As a result a number of on-line blade vibration measurement techniques are available, each with its own associated advantages and shortcomings. In general, on-blade sensor measurement techniques suffer from sensor lifespan, whereas non-contact techniques usually have measurement bandwidth limitations. One non-contact measurement technique that yields improvements in the area of measurement bandwidth is laser Doppler vibrometry. This thesis presents results and findings from utilizing laser Doppler vibrometry in an Eulerian fashion (i.e. a fixed reference frame) to measure on-line blade vibrations in axial-flow turbomachinery. With this measurement approach, the laser beam is focussed at a fixed point in space and measurements are available for the periods during which each blade sweeps through the beam. The characteristics of the measurement technique are studied analytically with an Euler-Bernoulli cantilever beam and experimental verification is performed. An approach for the numerical simulation of the measurement technique is then presented. Associated with the presented measurement technique are the short periods during which each blade is exposed to the laser beam. This characteristic yields traditional frequency domain signal processing techniques unsuitable for providing useful blade health indicators. To obtain frequency domain information from such short signals, it is necessary to employ non-standard signal processing techniques such as non-harmonic Fourier analysis. Results from experimental testing on a single-blade test rotor at a single rotor speed are presented in the form of phase angle trends obtained with non-harmonic Fourier analysis. Considering the maximum of absolute unwrapped phase angle trends around various reference frequencies, good indicators of blade health deterioration were obtained. These indicators were verified numerically. To extend the application of this condition monitoring approach, measurements were repeated on a five-blade test rotor at four different rotor speeds. Various damage cases were considered as well as different ELDV measurement positions. Using statistical parameters of the abovementioned indicators as well as time domain parameters, it is shown that with this condition monitoring approach, blade damage can successfully be identified and quantified with the aid of artificial neural networks. / Thesis (PhD)--University of Pretoria, 2010. / Mechanical and Aeronautical Engineering / unrestricted

In der vorliegenden Arbeit werden der Entwurf, die Technologie und die Parameteridentifikation von Silizium basierten mikroelektromechanischen Systemen (MEMS) mit piezoelektrischen Dünnschicht-Aluminiumnitrid (AlN) vorgestellt. Auf Basis des AlNs als elektromechanischer Wandler erfolgt die Fertigung eines MEMS Technologiedemonstrators für energiearme Inertialsensoren. Das AlN wird über einen reaktiven Sputterprozess auf einer Wachstumsschicht abgeschieden. Durch Parametervariation des reaktiven Sputterprozesses und der Wachstumsschicht werden die piezoelektrischen Eigenschaften des AlNs optimiert. Die Entwicklung einer Gesamttechnologie führt zu einer Integration des Dünnschicht-AlNs in Silizium-Mikromechaniken. Die Röntgenbeugung (XRD) ermöglicht die Kristallstruktur des AlNs zu qualifizieren. Darüber hinaus werden weitere Analysemethoden vorgestellt, die eine hoch genaue und reproduzierbare messtechnische Bestimmung der piezoelektrischen Koeffizienten aus mikromechanischen Messstrukturen ermöglichen. Die Determination der piezoelektrischen Koeffizienten des Dünnschicht-AlNs aus den Messstrukturen erfolgt mittels analytischen und FE Modellen sowie der Laser-Doppler-Vibrometrie (LDV). Der Fokus der Arbeit liegt hierbei auf der Identifikation der longitudinalen und transversalen piezoelektrischen Ladungskoeffizienten des AlNs. Als Technologiedemonstrator wird ein einachsiger Inertialsensor mit integriertem piezoelektrischen Dünnschicht-AlN vorgestellt. Das MEMS generiert aufgrund des piezoelektrischen Wandlers intrinsisch elektrische Ladungen bei Einwirkung einer mechanischen Energie. Dadurch ist keine elektrische Energiezufuhr für die Messung eines inertialen Ereignisses notwendig. Der vorgestellte Demonstrator wird hinsichtlich seiner Ladungs- und Spannungssensitivität optimiert. Zur theoretischen Beschreibung der Funktionsweise werden analytische, sowie FE und SPICE Modelle genutzt. Eine Charakterisierung des MEMS Bauelements erfolgt hinsichtlich der mechanischen und elektrischen Eigenschaften. / The thesis includes the design, the technology and the parameter identification of silicon-based microelectromechanical systems (MEMS) with piezoelectric thin film of aluminum nitride (AlN). A low-energy inertial sensor as technology demonstrator based on AlN as an electromechanical transducer a MEMS manufacturing process is shown. The AlN is deposited via a reactive sputtering on a growth layer. By varying parameters of the reactive sputtering and the growth layer of AlN, the piezoelectric properties can be optimized. The development of an overall technology results to an integration of the thin film AlNs in silicon micromechanics. X-ray diffraction (XRD) allows to qualify the crystal structure of AlN. Further methods are developed that enable a highly accurate and repeatable metrological determination of piezoelectric coefficients measurement structures. The determination of piezoelectric coefficients of the thin film AlN from the measurement structures is resulting from analytical methods and FE models and the laser Doppler vibrometry (LDV). The identification of the longitudinal and transverse piezoelectric charge coefficient of AlN is one main focus of this work. A uniaxial inertial sensor with an integrated piezoelectric thin film of AlN is presented as technology demonstrator. The piezoelectric transducer of the MEMS is generating electric charges intrinsically as reaction of mechanical stress. Thus, no electric power supply for the measurement of an inertial event is necessary. The presented demonstrator has been optimized with respect to its charge and voltage sensitivity. For a theoretical description analytical and FE and SPICE models are used. A characterization of the MEMS device is carried out with regard to the mechanical and electrical properties.

In der vorliegenden Arbeit wird eine Methode zur Charakterisierung von Mikrosystemen mit beweglichen Komponenten dargestellt. Sie erlaubt, funktionsrelevante Parameter und deren Schwankungen produktionsbegleitend auf Waferlevel zu ermitteln. Dabei wird vorausgesetzt, dass die Sollform der Struktur und die Abweichungsarten bekannt sind. Die Methode beruht auf dem Vergleich von numerisch berechneten mit experimentell ermittelten Eigenfrequenzen der untersuchten Mikrosysteme. Dazu wird die Abhängigkeit verschiedener Eigenfrequenzen von den gesuchten Parametern mittels einer Parametervariationsanalyse berechnet und durch eine geeignete Funktion angenähert. Die Messung der dynamischen Eigenschaften erfolgt mit Hilfe eines Bewegungsanalysators, der auf einem Laser-Doppler-Vibrometer basiert. Im letzen Schritt werden die gesuchten Parameter berechnet. Kernpunkt der entwickelten Methode sind Messungen auf der Basis von speziellen Teststrukturen, die im Waferlayout neben den eigentlichen Nutzstrukturen platziert sind und parallel mit den Nutzstrukturen prozessiert werden. Es werden Algorithmen zur Generierung des Designs der Teststrukturen und ihrer Platzierung im Waferlayout entwickelt. Dabei werden das Design der Nutzstruktur und deren funktionsrelevante Parameter, der technologische Ablauf und materialspezifische Kennwerte berücksichtigt. Im Ergebnis liegt eine Bibliothek von Standard-Teststrukturen vor, die für produktionsbegleitende Messungen sowie für die Übertragbarkeit der Ergebnisse geeignet sind. Außerdem werden allgemeingültige Richtlinien zur Durchführung der Messungen an den Standard-Teststrukturen abgeleitet. Das Messverfahren wurde an unterschiedlichen Mikrosystemen mit beweglichen Komponenten überprüft und zu einer allgemeinen Messmethode für diese Klasse von Mikrosystemen erweitert. / In this work a method for the characterization of microsystems with movable components is presented. The method allows to determine the relevant parameters and their variations on wafer level if the nominal shape of the structure and the type of deviations are known. The method is based on a comparison of the numerically calculated and experimentally measured Eigenfrequencies of the microsystems. For that purpose, the relationships between various Eigenfrequencies and the searched parameters are calculated by parameter variation analysis and the results of this analysis are approximated with appropriate functions. A Laser Doppler vibrometer based motion analyzer is used to determine the frequency response function of the micromechanical structure and extract Eigenfrequencies. The comparison of the measured and the calculated frequencies provides values for the searched parameters. The key element of the developed method is the measurement on special test structures that are placed in the wafer layout next to the actual microsystems and processed in the same technological process parallel to the actual microsystems. Algorithms for designing the test structures and their placement in the wafer layout are shown, taking into account the design of the actual microsystems and the function parameters of the technological process as well as material characteristics. As a result, a library of standard test structures for function relevant parameters is available. A general guideline for the measurement on the test structures is presented. The presented method is verified on various microsystems and extended to a whole class of microsystems with movable components.

In der vorliegenden Arbeit werden der Entwurf, die Technologie und die Parameteridentifikation von Silizium basierten mikroelektromechanischen Systemen (MEMS) mit piezoelektrischen Dünnschicht-Aluminiumnitrid (AlN) vorgestellt. Auf Basis des AlNs als elektromechanischer Wandler erfolgt die Fertigung eines MEMS Technologiedemonstrators für energiearme Inertialsensoren. Das AlN wird über einen reaktiven Sputterprozess auf einer Wachstumsschicht abgeschieden. Durch Parametervariation des reaktiven Sputterprozesses und der Wachstumsschicht werden die piezoelektrischen Eigenschaften des AlNs optimiert. Die Entwicklung einer Gesamttechnologie führt zu einer Integration des Dünnschicht-AlNs in Silizium-Mikromechaniken. Die Röntgenbeugung (XRD) ermöglicht die Kristallstruktur des AlNs zu qualifizieren. Darüber hinaus werden weitere Analysemethoden vorgestellt, die eine hoch genaue und reproduzierbare messtechnische Bestimmung der piezoelektrischen Koeffizienten aus mikromechanischen Messstrukturen ermöglichen. Die Determination der piezoelektrischen Koeffizienten des Dünnschicht-AlNs aus den Messstrukturen erfolgt mittels analytischen und FE Modellen sowie der Laser-Doppler-Vibrometrie (LDV). Der Fokus der Arbeit liegt hierbei auf der Identifikation der longitudinalen und transversalen piezoelektrischen Ladungskoeffizienten des AlNs. Als Technologiedemonstrator wird ein einachsiger Inertialsensor mit integriertem piezoelektrischen Dünnschicht-AlN vorgestellt. Das MEMS generiert aufgrund des piezoelektrischen Wandlers intrinsisch elektrische Ladungen bei Einwirkung einer mechanischen Energie. Dadurch ist keine elektrische Energiezufuhr für die Messung eines inertialen Ereignisses notwendig. Der vorgestellte Demonstrator wird hinsichtlich seiner Ladungs- und Spannungssensitivität optimiert. Zur theoretischen Beschreibung der Funktionsweise werden analytische, sowie FE und SPICE Modelle genutzt. Eine Charakterisierung des MEMS Bauelements erfolgt hinsichtlich der mechanischen und elektrischen Eigenschaften. / The thesis includes the design, the technology and the parameter identification of silicon-based microelectromechanical systems (MEMS) with piezoelectric thin film of aluminum nitride (AlN). A low-energy inertial sensor as technology demonstrator based on AlN as an electromechanical transducer a MEMS manufacturing process is shown. The AlN is deposited via a reactive sputtering on a growth layer. By varying parameters of the reactive sputtering and the growth layer of AlN, the piezoelectric properties can be optimized. The development of an overall technology results to an integration of the thin film AlNs in silicon micromechanics. X-ray diffraction (XRD) allows to qualify the crystal structure of AlN. Further methods are developed that enable a highly accurate and repeatable metrological determination of piezoelectric coefficients measurement structures. The determination of piezoelectric coefficients of the thin film AlN from the measurement structures is resulting from analytical methods and FE models and the laser Doppler vibrometry (LDV). The identification of the longitudinal and transverse piezoelectric charge coefficient of AlN is one main focus of this work. A uniaxial inertial sensor with an integrated piezoelectric thin film of AlN is presented as technology demonstrator. The piezoelectric transducer of the MEMS is generating electric charges intrinsically as reaction of mechanical stress. Thus, no electric power supply for the measurement of an inertial event is necessary. The presented demonstrator has been optimized with respect to its charge and voltage sensitivity. For a theoretical description analytical and FE and SPICE models are used. A characterization of the MEMS device is carried out with regard to the mechanical and electrical properties.

[ES] En un presente marcado por la continua lucha contra la contaminación y el cambio climático, la investigación en mejoras tecnológicas que permitan una transición aceptable para la sociedad hacia un futuro más ecológico ocupa un papel fundamental. En concreto, la aviación es un foco constante de innovación, ya que es considerada una función indispensable en una sociedad tan globalizada como la actual, pero con unos niveles de contaminación preocupantes. En este aspecto, el desarrollo de motores con altas eficiencias es un paso clave para la transición medioambiental. Sin embargo, estas alternativas presentan un reto tecnológico en cuanto a su gestión térmica basado, principalmente, en la necesidad de aumentar la refrigeración. En este contexto e impulsada por el proyecto "Aerodynamic upgrade of Surface Air Cooled Oil Cooler (SACOC)" de Clean Sky 2, esta tesis doctoral se centra en el estudio experimental de geometrías de intercambiadores de calor de superficie para la refrigeración del aceite motor mediante el uso del aire del flujo secundario del turbofan. Actualmente, existen una serie de limitaciones en cuanto a las capacidades para llevar a cabo un análisis y diseño detallado de este tipo de intercambiadores de calor debido a la falta de instalaciones que permitan un correcta, completa y robusta caracterización experimental. Las principales fuentes de datos se basan en cálculos numéricos validados a partir de extrapolaciones en condiciones de cuestionable aplicabilidad. A lo largo de la tesis se presentan los resultados obtenidos tras una detallada caracterización de cuatro diferentes geometrías de intercambiadores de calor empleando tanto técnicas intrusivas como ópticas. Se utiliza un banco de flujo capaz de generar una corriente de aire típica alrededor de los intercambiadores, mientras que un sistema de acondicionamiento de aceite controla el punto de operación por el lado caliente. Para recrear de manera más realista las condiciones de funcionamiento, se presenta una metodología para generar de manera automática pantallas de distorsión que pueden reproducir una distribución bidimensional de velocidades objetivo mediante la manufactura aditiva de paneles de porosidad variable. Este modelo, analizado mediante CFD y validado experimentalmente, se utiliza para reproducir el perfil de velocidades típico presente en torno al intercambiador en una circunstancia real de operación. Tras definir métricas relevantes que permitan analizar el comportamiento de las distintas geometrías, se llega a la conclusión de que los problemas aerodinámico y térmico están altamente acoplados en estos dispositivos, demostrando la necesidad de un cuidadoso diseño para mejorar las actuaciones del intercambiador. Los resultados muestran que puede llegar a obtenerse una mejora de más de un 12% en la caída de presión y casi un 20% en el intercambio de calor. Además, se ha confirmado el impacto del uso de la pantalla de distorsión, con variaciones del orden de 10% en ambas variables. Los resultados también muestran que es posible realizar una caracterización preliminar de manera fiable con un modelo impreso en 3D, en cuanto campos de velocidades, pérdidas de presión y frecuencias propias corregidas. Con el análisis llevado a cabo en esta tesis, se puede concluir que es fundamental tener una instalación experimental que reproduzca las condiciones de funcionamiento reales de un motor para realizar estudios relevantes de intercambiadores de calor. Además, es necesario el uso de métricas adecuadas junto con el desarrollo de una metodología exhaustiva, fiable y robusta. Los resultados y metodología presentados en en esta investigación pueden llegar a tener un impacto importante tanto a nivel académico como industrial, ya que abren la puerta a desarrollar sistemas de gestión térmica más eficiente en unas etapas de diseño preliminares que son más asequibles económicamente, consumen menos tiempo y tienen mayor flexibilidad para introducir modificaciones. / [CAT] En un present marcat per la lluita contínua contra la contaminació i el canvi climàtic, la recerca en millores tecnològiques que permetin una transició acceptable per a la societat cap a un futur més ecològic ocupa un paper fonamental. En concret, l'aviació és un focus constant d'innovació, ja que és considerada una funció indispensable en una societat tan globalitzada com l'actual però amb uns nivells de contaminació preocupants. En aquest aspecte, el desenvolupament de motors amb altes eficiències és un pas clau per a la transició mediambiental. Tot i això, aquestes alternatives presenten un repte tecnològic quant a la seva gestió tèrmica basat, principalment, en la necessitat d'augmentar la refrigeració. En aquest context i impulsada pel projecte "Aerodynamic upgrade of Surface Air Cooled Oil Cooler (SACOC)" de Clean Sky 2, aquesta tesi doctoral se centra en l'estudi experimental de geometries d'intercanviadors de calor de superfície per a la refrigeració de l'oli motor mitjançant l'ús de l'aire del flux secundari del turbofan. Actualment, hi ha una sèrie de limitacions quant a les capacitats per dur a terme una anàlisi i disseny detallat d'aquest tipus d'intercanviadors de calor a causa de la manca d'instal·lacions que permetin una caracterització experimental correcta, completa i robusta. Les fonts de dades principals es basen en càlculs numèrics validats a partir d'extrapolacions en condicions de qüestionable aplicabilitat. Al llarg de la tesi es presenten els resultats obtinguts després d'una detallada caracterització de quatre geometries diferents d'intercanviadors de calor emprant tant tècniques intrusives com òptiques. Sutilitza un banc de flux capaç de generar un corrent daire típic al voltant dels intercanviadors, mentre que un sistema de condicionament doli controla el punt doperació pel costat calent. Per recrear de manera més realista les condicions de funcionament, es presenta una metodologia per generar de manera automàtica pantalles de distorsió que poden reproduir una distribució bidimensional de velocitats objectiu mitjançant la manufactura additiva de panells de porositat variable. Aquest model, analitzat mitjançant CFD i validat experimentalment, sutilitza per reproduir el perfil de velocitats típic present al voltant de lintercanviador en una circumstància real doperació. Després de definir mètriques rellevants que permetin analitzar el comportament de les diferents geometries, s'arriba a la conclusió que els problemes aerodinàmic i tèrmic estan altament acoblats en aquests dispositius, demostrant la necessitat d'un disseny acurat per millorar les actuacions de l'intercanviador. Els resultats mostren que es pot arribar a obtenir una millora de més d'un 12% a la caiguda de pressió i gairebé un 20% a l'intercanvi de calor. A més, s'ha confirmat l'impacte de l'ús de la pantalla de distorsió, amb variacions de l'ordre del 10% a les dues variables. Els resultats també mostren que és possible fer una caracterització preliminar de manera fiable amb un model imprès en 3D, en tant que camps de velocitats, pèrdues de pressió i freqüències pròpies corregides. Amb l'anàlisi duta a terme en aquesta tesi, es pot concloure que és fonamental tenir una instal·lació experimental que reprodueixi les condicions de funcionament reals d'un motor per fer estudis rellevants d'intercanviadors de calor. A més, cal fer servir mètriques adequades juntament amb el desenvolupament d'una metodologia exhaustiva, fiable i robusta. Els resultats i metodologia presentats en aquesta investigació poden arribar a tenir un impacte important tant a nivell acadèmic com industrial, ja que obren la porta a desenvolupar sistemes de gestió tèrmica més eficient en unes etapes de disseny preliminars que són més assequibles econòmicament, consumeixen menys temps i tenen més flexibilitat per introduir modificacions. / [EN] In a present marked by the continuous fight against pollution and climate change, research into technological improvements that allow an acceptable transition for society towards a greener future occupies a fundamental role. Specifically, aviation is a constant focus of innovation, since it is considered an essential function in a society as globalized as today's, but with worrying levels of pollution. In this regard, the development of motors with high efficiencies is a key step for the environmental transition. However, these alternatives present a technological challenge in terms of their thermal management, based mainly on the need to increase cooling. In this context and promoted by the Clean Sky 2 "Aerodynamic upgrade of Surface Air Cooled Oil Cooler (SACOC)" project, this doctoral thesis focuses on the experimental study of surface heat exchanger geometries for engine oil cooling using the use of secondary flow air from the turbofan. Currently, there are a number of limitations regarding the capacity to carry out a detailed analysis and design of this type of heat exchanger due to the lack of facilities that allow a correct, complete and robust experimental characterization. The main data sources are based on numerical calculations validated from extrapolations under conditions of questionable applicability. The thesis presents results after a detailed characterization of four different geometries of heat exchangers using both intrusive and optical techniques. A flow bench capable of generating a typical air current around the exchangers is used, while an oil conditioning system controls the point of operation on the hot side. To more realistically recreate operating conditions, a methodology is presented to automatically generate distortion screens that can reproduce a two-dimensional distribution of target velocities through additive manufacturing of variable porosity panels. This model, analyzed by means of CFD and validated experimentally, is used to reproduce the typical speed profile present around the exchanger in a real operating circumstance. After defining relevant metrics that allow analyzing the behaviour of the different geometries, it is concluded that aerodynamic and thermal problems are highly coupled in these devices, demonstrating the need for careful design to improve the exchanger's performance. The results show that an improvement of more than 12% in pressure drop and almost 20% in heat exchange can be obtained. In addition, the impact of using the distortion screen has been confirmed, with variations of the order of 10% in both variables. The results also show that it is possible to carry out a preliminary characterization in a reliable way with a 3D printed model, in terms of velocity fields, pressure losses and corrected eigenfrequencies. With the analysis carried out in this thesis, it can be concluded that it is essential to have an experimental installation that reproduces the real operating conditions of an engine to carry out relevant studies of heat exchangers. In addition, the use of appropriate metrics is necessary together with the development of a comprehensive, reliable and robust methodology. The results and methodology presented in this research can have a significant impact both at an academic and industrial level, since they open the door to developing more efficient thermal management systems in preliminary design stages that are more affordable, consume less time and have more flexibility to make changes. / The respondent wishes to acknowledge the financial support received through the Programa de Apoyo para la Investigación y Desarrollo (PAID) of Univer- sitat Politècnica de València under grant PAID-01-20 n◦ 21589. This project has received funding from the Clean Sky 2 Joint Undertak- ing under the European Unions Horizon 2020 research and innovation pro- gramme under grant agreement No 831977 Aerodynamic upgrade of Sur- face Air-Cooled Oil Coolers (SACOC) / Felgueroso Rodríguez, A. (2023). Aerothermal Characterisation of Surface Heat Exchangers for Turbofans [Tesis doctoral]. Universitat Politècnica de València. https://doi.org/10.4995/Thesis/10251/195852