Bomb-tritium input function calculated from the details of the nuclear atmospheric bomb tests released by the UNSCEAR [2000]

Improving the representation of the hydrological cycle in Atmospheric General Circulation Models (AGCMs) is one of the main challenges in modeling the Earth's climate system. One way to evaluate model performance is to simulate the transport of water isotopes. Among those available, tritium (HTO) is an extremely valuable tracer, because its content in the different reservoirs involved in the water cycle (stratosphere, troposphere, ocean) varies by order of magnitude. Previous work incorporated natural tritium into LMDZ-iso, a version of the LMDZ general circulation model enhanced by water isotope diagnostics. Here for the first time, the anthropogenic tritium injected by each of the atmospheric nuclear-bomb tests between 1945 and 1980 has been first estimated and further implemented in the model; it creates an opportunity to evaluate certain aspects of LDMZ over several decades by following the bomb-tritium transient signal through the hydrological cycle. Simulations of tritium in water vapor and precipitation for the period 1950-2008, with both natural and anthropogenic components, are presented in this study. LMDZ-iso satisfactorily reproduces the general shape of the temporal evolution of tritium. However, LMDZ-iso simulates too high a bomb-tritium peak followed by too strong a decrease of tritium in precipitation. The too diffusive vertical advection in AGCMs crucially affects the residence time of tritium in the stratosphere. This insight into model performance demonstrates that the implementation of tritium in an AGCM provides a new and valuable test of the modeled atmospheric transport, complementing water stable isotope modeling.

Mise en valeur des résidus du concentrateur de la mine Niobec par la flottaison de l’apatite

L’usine Niobec traite un minerai de pyrochlore porteur de niobium pour produire le ferro-niobium utilisé pour la fabrication d’acier. L’usine récupère environ 60% des minéraux de niobium. Les rejets contiennent du niobium et d’autres espèces minérales potentiellement valorisables. Les travaux présentés dans ce mémoire visent à identifier les espèces pouvant être valorisées dans les rejets de Niobec dont les plus prometteurs sont les éléments de terres rares, les minéraux de niobium et l’apatite. Dans le but de concentrer l’apatite des rejets de l’usine, une analyse chimique des rejets a permis de cibler comme flux d’intérêt les particules de dimension supérieure à 0,038mm dans le concentré de carbonates et les rejets du circuit de flottation du pyrochlore. La méthode utilisée pour valoriser les phosphates est la flottation. Les meilleurs résultats ont été obtenus par flottation directe des minéraux de phosphate du concentré de carbonates dans les rejets de Niobec. Le collecteur utilisé est un acide gras de type AERO 6493 avec un mélange d’amidon de tapioca et de NaOH utilisé comme déprimant pour les carbonates. Ces conditions ont permis de produire un concentré d’apatite titrant entre 30 à 32 % P2O5 avec un rendement de 50 à 60% du P2O5 contenue dans le concentré de carbonates. La teneur en MgO dans le concentré d’apatite est comprise entre 3 et 4% comparativement à 15% dans l’alimentation. Puisque le MgO est principalement associé à la dolomie ces résultats confirment une bonne dépression de ce minéral lors de la flottation de l’apatite du concentré de carbonates. La flottation de l’apatite à partir des rejets du pyrochlore n’a pas permis d’obtenir un concentré de valeur commerciale. Le meilleur résultat obtenu lors des essais de flottation sur les rejets pyrochlore correspond à une teneur de 14%avec un rendement de 53% P2O5. Les résultats obtenus montrent toutefois le potentiel associé à la récupération des minéraux de phosphates et justifient la poursuite des travaux, cette fois, moins exploratoires que les travaux rapportés dans ce mémoire.

Interview with Hans G. Hornung

An interview in two sessions, June and July 2014, with Hans Georg Hornung, Clarence L. Johnson Professor of Aeronautics, emeritus, in the Division of Engineering and Applied Science. Dr. Hornung describes the origins of the German Templer Colony in Palestine and his upbringing there before and during World War II. Family moves to Templer settlement, Melbourne, Australia, 1948. He attends technical college; University of Melbourne; master’s in engineering, 1962. Researcher, Aeronautical Research Laboratories, Melbourne; PhD, Imperial College, London, 1965. He recalls his academic career at the Australian National University, Canberra (1967-1980); his interest in hypersonics; building free-piston shock tunnel with Raymond Stalker. Sabbatical in Darmstadt with Ernst Becker. Seven years as director of fluid-mechanics institute of the DLR [Deutsches Zentrum für Luft- und Raumfahrt], in Göttingen. Comes to Caltech in 1987 to succeed Hans W. Liepmann as director of GALCIT [Graduate Aerospace Laboratories, California Institute of Technology]. Recalls his various aero colleagues, his work with Rocketdyne on Caltech’s T5 (successor to Canberra’s T3 shock tunnel) and Ludwieg tube, collaboration with JPL on space program, and work with graduate students Simon Sanderson and Eric Cummings. Discusses his involvement in various scientific societies and his current activities and continuing research as an emeritus professor.

Combustion Instability and Active Control: Alternative Fuels, Augmentors, and Modeling Heat Release

Experimental and analytical studies were conducted to explore thermo-acoustic coupling during the onset of combustion instability in various air-breathing combustor configurations. These include a laboratory-scale 200-kW dump combustor and a 100-kW augmentor featuring a v-gutter flame holder. They were used to simulate main combustion chambers and afterburners in aero engines, respectively. The three primary themes of this work includes: 1) modeling heat release fluctuations for stability analysis, 2) conducting active combustion control with alternative fuels, and 3) demonstrating practical active control for augmentor instability suppression. The phenomenon of combustion instabilities remains an unsolved problem in propulsion engines, mainly because of the difficulty in predicting the fluctuating component of heat release without extensive testing. A hybrid model was developed to describe both the temporal and spatial variations in dynamic heat release, using a separation of variables approach that requires only a limited amount of experimental data. The use of sinusoidal basis functions further reduced the amount of data required. When the mean heat release behavior is known, the only experimental data needed for detailed stability analysis is one instantaneous picture of heat release at the peak pressure phase. This model was successfully tested in the dump combustor experiments, reproducing the correct sign of the overall Rayleigh index as well as the remarkably accurate spatial distribution pattern of fluctuating heat release. Active combustion control was explored for fuel-flexible combustor operation using twelve different jet fuels including bio-synthetic and Fischer-Tropsch types. Analysis done using an actuated spray combustion model revealed that the combustion response times of these fuels were similar. Combined with experimental spray characterizations, this suggested that controller performance should remain effective with various alternative fuels. Active control experiments validated this analysis while demonstrating 50-70\% reduction in the peak spectral amplitude. A new model augmentor was built and tested for combustion dynamics using schlieren and chemiluminescence techniques. Novel active control techniques including pulsed air injection were implemented and the results were compared with the pulsed fuel injection approach. The pulsed injection of secondary air worked just as effectively for suppressing the augmentor instability, setting up the possibility of more efficient actuation strategy.

Otosclerose: resultados audiométricos 5 anos após cirurgia estapédica

Objetivo: Avaliar os resultados audiométricos, 5 anos após estapedectomia, numa série de 85 ouvidos. Desenho do estudo: Retrospetivo Materiais e métodos: Análise dos resultados audiométricos obtidos aos 5 anos após estapedectomia e comparação com os valores do pré-operatório e pós-operatório precoce. Resultados: Cinco anos após estapedectomia observou-se encerramento do gap aero-ósseo para valores ≤ 10 dB em 74% dos ouvidos. Nove doentes foram submetidos a revisão cirúrgica. Seis apresentavam gap aero-ósseo > 20 dB, recusando revisão cirúrgica. O gap aero-ósseo médio aos 5 anos era de 7,17 dB, representando um ganho auditivo de 21,28 dB em relação ao pré-operatório e um aumento do gap de 2,85 dB em relação ao pós-operatório precoce. Conclusões: Os nossos resultados audiométricos 5 anos após estapedectomia são satisfatórios e coincidentes com a literatura. A estapedectomia representa uma solução eficaz na otosclerose apresentando, na grande maioria dos casos, resultados estáveis ao longo do tempo.

Resultados de cirurgia estapédica: a experiência recente do Hospital Professor Doutor Fernando Fonseca

Objectivo: analisar a experiência recente em cirurgia estapédica do Hospital Professor Doutor Fernando Fonseca, recorrendo à avaliação dos seus resultados audiométricos. Materiais e métodos: avaliação retrospectiva de processos clínicos referentes a 155 cirurgias estapédicas consecutivas realizadas no Hospital Professor Doutor Fernando Fonseca, entre Janeiro de 2006 e Dezembro de 2010. Resultados: a média de idades foi de 43,6 anos. A média de 4 frequências (0.5, 1, 2 e 4 kHz) do gap aero-ósseo pós- operatório foi de 5,2 dB. O ganho auditivo médio registado foi de 27 dB sendo a taxa de sucesso cirúrgico de 88,2%. A alteração da condução óssea nas altas frequências foi de 4,9 dB. Conclusões: A cirurgia estapédica apresenta uma elevada taxa de sucesso e baixa frequência de complicações, sendo uma opção preferencial no tratamento da otosclerose. Os resultados deste trabalho confirmam-no reforçando o recurso à cirurgia estapédica no Hospital Professor Doutor Fernando Fonseca.

Non-contact test set-up for aeroelasticity in a rotating turbomachine combining a novel acoustic excitation system with tip-timing

Due to trends in aero-design, aeroelasticity becomes increasingly important in modern turbomachines. Design requirements of turbomachines lead to the development of high aspect ratio blades and blade integral disc designs (blisks), which are especially prone to complex modes of vibration. Therefore, experimental investigations yielding high quality data are required for improving the understanding of aeroelastic effects in turbomachines. One possibility to achieve high quality data is to excite and measure blade vibrations in turbomachines. The major requirement for blade excitation and blade vibration measurements is to minimize interference with the aeroelastic effects to be investigated. Thus in this paper, a non-contact-and thus low interference-experimental set-up for exciting and measuring blade vibrations is proposed and shown to work. A novel acoustic system excites rotor blade vibrations, which are measured with an optical tip-timing system. By performing measurements in an axial compressor, the potential of the acoustic excitation method for investigating aeroelastic effects is explored. The basic principle of this method is described and proven through the analysis of blade responses at different acoustic excitation frequencies and at different rotational speeds. To verify the accuracy of the tip-timing system, amplitudes measured by tip-timing are compared with strain gage measurements. They are found to agree well. Two approaches to vary the nodal diameter (ND) of the excited vibration mode by controlling the acoustic excitation are presented. By combining the different excitable acoustic modes with a phase-lag control, each ND of the investigated 30 blade rotor can be excited individually. This feature of the present acoustic excitation system is of great benefit to aeroelastic investigations and represents one of the main advantages over other excitation methods proposed in the past. In future studies, the acoustic excitation method will be used to investigate aeroelastic effects in high-speed turbomachines in detail. The results of these investigations are to be used to improve the aeroelastic design of modern turbomachines.

From genes to radioresistance in head and neck squamous cell carcinoma

Head and Neck Cancers (HNC) are a group of tumours located in the upper aero-digestive tract. Head and Neck Squamous Cell Carcinoma (HNSCC) represent about 90% of all HNC cases. It has been considered the sixth most malignant tumour worldwide and, despite clinical and technological advances, the five-year survival rate has not improved much in the last years. Nowadays, HNSCC is well established as a heterogeneous disease and that its development is due to accumulation of genetic events. Apart from the majority of the patients being diagnosed in an advanced stage, HNSCC is also a disease with poor therapeutic outcome. One of the therapeutic approaches is radiotherapy. However, this approach has different drawbacks like the radioresistance acquired by some tumour cells, leading to a worse prognosis. A major knowledge in radiation biology is imperative to improve this type of treatment and avoid late toxicities, maintaining patient quality of life in the subsequent years after treatment. Then, identification of genetic markers associated to radiotherapy response in patients and possible alterations in cells after radiotherapy are essential steps towards an improved diagnosis, higher survival rate and a better life quality. Not much is known about the radiation effects on cells, so, the principal aim of this study was to contribute to a more extensive knowledge about radiation treatment in HNSCC. For this, two commercial cell lines, HSC-3 and BICR-10, were used and characterized resorting to karyotyping, aCGH and MS-MLPA. These cell lines were submitted to different doses of irradiation and the resulting genetic and methylation alterations were evaluated. Our results showed a great difference in radiation response between the two cell lines, allowing the conclusion that HSC-3 was much more radiosensitive than BICR-10. Bearing this in mind, analysis of cell death, cell cycle and DNA damages was performed to try to elucidate the motifs behind this difference. The characterization of both cell lines allowed the confirmation that HSC-3 was derived from a metastatic tumour and the hypothesis that BICR-10 was derived from a dysplasia. Furthermore, this pilot study enabled the suggestion of some genetic and epigenetic alterations that cells suffer after radiation treatment. Additionally, it also allowed the association of some genetic characteristics that could be related to the differences in radiation response observable in this two cell lines. Taken together all of our results contribute to a better understanding of radiation effects on HNSCC allowing one further step towards the prediction of patients’ outcome, better choice of treatment approaches and ultimately a better quality of life.

Teste Apercetivo Temático Aeronáutico

O Teste Apercetivo Temático Aeronáutico (TAT-AERO) é um teste projetivo utilizado na Força Aérea Portuguesa (FA) na avaliação psicológica prévia ao Programa de Dessensibilização do Enjoo Aeronáutico (PDEA). A presente investigação, norteada para o estudo do TAT-AERO aplicado ao PDEA, foi desenvolvida com recurso à metodologia de investigação qualitativa assente num método hipotético-dedutivo e num desenho de pesquisa comparativo. Tendo como pergunta de partida (PP) “Que aspetos do funcionamento emocional salientam as respostas dos protocolos TAT-AERO dos alunos de pilotagem que realizaram o PDEA e dos alunos de pilotagem sem sintomatologia ligada ao enjoo aeronáutico?”, passou pela aplicação do TAT-AERO a dois grupos de alunos de pilotagem. Em concreto, a um grupo que não apresentou sintomatologia ligada ao enjoo aeronáutico e a um outro grupo que, por ter apresentado esta sintomatologia, havia realizado o PDEA. Os dados obtidos da comparação dos protocolos destes dois grupos, revelaram a existência de diferenças entre os dois grupos de alunos de pilotagem (sem sintomatologia ligada ao enjoo aeronáutico e que haviam realizado o PDEA), em concreto na forma como lidam com a temática da morte, o conflito familiar e o seu distanciamento em relação à história que relatam. Abstract: The Thematic Apperception Aeronautical Test ( TAT- AERO ) is a projective test used in Portuguese Air Force in the previous psychological evaluation to Desensitization Program for Airsickness ( PDEA ). In present investigation, guided for the study of the TAT- AERO applied to PDEA, the research was developed using the qualitative research methodology based on a hypothetical-deductive method, the research design was comparative. The investigation had the departure question (PP) " What aspects of emotional functioning stress responses of TAT- AERO protocols of pilotage students who performed the PDEA and pilot students without symptoms linked to airsickness?" The TAT-AERO was applied to a group of pilot students have shown no symptoms linked to airsickness, and the respective protocols such as the protocols of pilotage students who performed the PDEA were compared in order to assess any specific each of the groups. The data revealed that there are differences between the two groups of students (without symptoms linked to airsickness and performed the PDEA) in the way they deal with the theme of death, family conflict and distancing itself from the story reported.

Energy-efficiency analysis of cluster-based routing protocols in wireless sensor network

This paper extends the conditions of the cluster-based routing protocols in terms of general algorithm complexity of data fusion, general compressing ratio of data fusion, and network area with long distance. Corresponding three general evaluation methods to evaluate the energy efficiency of the cluster-based routing protocols such as LEACH, PEGASIS, and BCDCP are provided. Moreover, three facts are found in them: (1) High-level software energy macro model is used to compute the energy dissipation of general data fusion software and make the constant value of energy dissipation of 1-bit data fusion an especial instance. (2) Multi-hop energy efficiency is related to the radio hardware parameters and the dynamic topology of network and the above protocols do not exploit the best use of the energy efficiency of multi-hop scheme. (3) High-energy dissipation non-cluster-head nodes, whose number changes with the density of the sensor nodes in clusters, worsen the death of nodes. The numerical results of experiments reprove these discoveries. Furthermore, they provide helpful guide for improving the above routing protocols to extent their application ranges.

ADVANCED COMPUTATIONAL MODELING OF THE INTERNAL STRUCTURE OF SMART WIND-TURBINE BLADES

Implementation of stable aeroelastic models with the ability to capture the complex features of Multi concept smartblades is a prime step in reducing the uncertainties that come along with blade dynamics. The numerical simulations of fluid structure interaction can thus be used to test a realistic scenarios comprising of full-scale blades at a reasonably low computational cost. A code which was a combination of two advanced numerical models was designed and was run with the help of paralell HPC supercomputer platform. The first model was based on a variation of dimensional reduction technique proposed by Hodges and Yu. This model was the one to record the structural response of heterogenous composite blades. This technique reduces the geometrical complexities of the heterogenous blade section into a stiffness matrix for an equivalent beam. This derived equivalent 1-D strain energy matrix is similar to the actual 3-D strain energy matrix in an asymptotic sense. As this 1-D matrix helps in accurately modeling the blade structure as a 1-D finite element problem, this substantially redues the computational effort and subsequently the computational cost that are required to model the structural dynamics at each step. Second model comprises of implementation of the Blade Element Momentum Theory. In this approach we map all the velocities and the forces with the help of orthogonal matrices that help in capturing the large deformations and the effects of rotations in calculating the aerodynamic forces. This ultimately helps us to take into account the complex flexo torsional deformations. In this thesis we have succesfully tested these computayinal tools developed by MTU’s research team lead by for the aero elastic analysis of wind-turbine blades. The validation in this thesis is majorly based on several experiments done on NREL-5MW blade, as this is widely accepted as a benchmark blade in the wind industry. Along with the use of this innovative model the internal blade structure was also changed to add up to the existing benefits of the already advanced numerical models.

El modelo de negocio en el desarrollo de una organización: un estudio de la compañía Southwest Airlines

El presente trabajo constituye una investigación acerca del rol del modelo de negocio en el desarrollo de las organizaciones. Esto se hace, en particular, a través del estudio detallado de la compañía Southwest Airlines. Se identifican para esta empresa, entre otros asuntos, las relaciones entre los recursos y los elementos que ofrece su entorno. Esto, en lo fundamental, para determinar el funcionamiento que ha llevado a la organización a la creación de un modelo de negocio adecuado y exitoso y el poder del mismo para evolucionar en un medio cambiante y aprovechar las oportunidades que este brinda. El presente documento presenta el origen, el desarrollo y los resultados de un estudio realizado a la empresa Southwest Airlines. En este se presentan sus políticas y estructura de procesos en relación con sus clientes —tanto internos como externos Esta se evidencia, al final, en la eficiencia, el compromiso de los empleados y otra serie de elementos que contribuyen al buen funcionamiento de la organización. El aporte de esta investigación está,en generar resultados a partir de un estudio a uno de los modelos de negocio de la industria aérea, específicamente el modelo de bajo costo (low cost). El propósito del trabajo fue desarrollar un análisis de las variables que consolidan todo el proceso de gestión en esta herramienta (business model) para ofrecerle al lector las pautas para fomentar la creación de modelos de negocio en las organizaciones y brindar así una estructura que contribuya a alcanzar el éxito en el mismo.