Rarefied gas dynamics: fundamentals, simulations and micro flows

Flight dynamics in Drosophila through a dynamically-scaled robotic approach

Flies are particularly adept at balancing the competing demands of delay tolerance, performance, and robustness during flight, which invites thoughtful examination of their multimodal feedback architecture. This dissertation examines stabilization requirements for inner-loop feedback strategies in the flapping flight of Drosophila, the fruit fly, against the backdrop of sensorimotor transformations present in the animal. Flies have evolved multiple specializations to reduce sensorimotor latency, but sensory delay during flight is still significant on the timescale of body dynamics. I explored the effect of sensor delay on flight stability and performance for yaw turns using a dynamically-scaled robot equipped with a real-time feedback system that performed active turns in response to measured yaw torque. The results show a fundamental tradeoff between sensor delay and permissible feedback gain, and suggest that fast mechanosensory feedback provides a source of active damping that compliments that contributed by passive effects. Presented in the context of these findings, a control architecture whereby a haltere-mediated inner-loop proportional controller provides damping for slower visually-mediated feedback is consistent with tethered-flight measurements, free-flight observations, and engineering design principles. Additionally, I investigated how flies adjust stroke features to regulate and stabilize level forward flight. The results suggest that few changes to hovering kinematics are actually required to meet steady-state lift and thrust requirements at different flight speeds, and the primary driver of equilibrium velocity is the aerodynamic pitch moment. This finding is consistent with prior hypotheses and observations regarding the relationship between body pitch and flight speed in fruit flies. The results also show that the dynamics may be stabilized with additional pitch damping, but the magnitude of required damping increases with flight speed. I posit that differences in stroke deviation between the upstroke and downstroke might play a critical role in this stabilization. Fast mechanosensory feedback of the pitch rate could enable active damping, which would inherently exhibit gain scheduling with flight speed if pitch torque is regulated by adjusting stroke deviation. Such a control scheme would provide an elegant solution for flight stabilization across a wide range of flight speeds.

Design support for turbomachinery

From the steam turbines which provide most of our electricity to the jet engines which have shrunk our World, turbomachines undoubtedly play a major role in life today. Competition in the turbomachinery industry is fiercely strong [Wisler, 1998], hence good aerodynamic design is vital. However, with efficiency levels already close to their theoretical maxima, companies are increasingly looking to reduce costs and increase reliability through improved design practice. Computational Fluid Dynamics (CFD) can make a strong contribution to assisting this process as it has the potential to increase performance while reducing cost. The situation is, however, complicated by an ever decreasing number of engineers with sufficient design experience to reap the full benefits offered by CFD. With the large risks involved, novice designers of today are increasingly confined to refining old designs rather than gaining experience, like their forebears, through 'clean sheet' exercises. Hence it is desirable to capture the knowledge and experience of older designers, before it is lost, to assist the engineers of tomorrow. It is therefore the aim of this project to produce a design support tool which will not only store the appropriate CFD codes, but also provide a dynamic signpost (based on elicited knowledge and experience) to advise the engineer in their use. The signposting methodology developed for the aerospace industry [Clarkson and Hamilton, 1997] will provide the basic framework for the tool. This paper reviews current turbomachinery design practice (including an examination of the relevant CFD) in order to establish the important issues which a support tool must address. Current design support methodologies and their propriety are then reviewed, followed by a detailed description of the signposting concept. It then sets out a clear statement of the objectives for the research and the methods proposed to meet them. The paper concludes with a timetable of the work.

Diseño de un aerogenerador de muy baja potencia para la alimentación de sistemas eléctricos aislados

[ES]En este Proyecto se desarrolla el diseño y la optimización de un aerogenerador de muy pequeña potencia enfocado a alimentar sistemas eléctricos aislados; concretamente, un sistema de iluminación. Se analizan todos los componentes del sistema aerogenerador, comparando las diversas alternativas posibles y eligiendo soluciones sencillas, baratas y eficientes para cada uno de ellos. Asimismo, se lleva a cabo un primer dimensionamiento de los mismos. El esfuerzo de diseño se ha centrado en las palas, por considerarse el componente más crítico y menos normalizado. Se han estudiado herramientas para su análisis detallado y su optimización desde el punto de vista aerodinámico, y éstas han sido implementadas en Matlab. Esto ha permitido generar un diseño óptimo ajustado a las necesidades del sistema. Asimismo, se han realizado las correspondientes tareas de planificación, analizado los múltiples beneficios de tipo técnico, económico, social y ambiental que la ejecución del presente Proyecto reportará, haciendo una programación completa del mismo y un análisis de los costes que supondrá.

Lehiaketako motor baten erditxasiaren diseinua

[EU]Proiektu honek lehiaketarako moto baten erditxasia garatzen du, baita txasira lotuta egongo den modua ere. Erditxasia pieza estruktural bat da eta nahiz eta agian beharrezkoa ez izan lehiaketako moto batean, izan ere hauetan pilotuek ipurdia oso aurrean kokatzen dute pisua txasira bideratuz, moto guztiek duten atal bat da eta pertsonaren pisua eta honek egiturari eragiten dizkion indar eta esfortzuak eusteko erabiltzen da. Kasu batzuetan txasiaren beraren barnean egoten da zati hau eta beraz dena pieza bat izaten da, baina gure kasuan biak, erditxasia eta txasia elkarri lotuta egongo dira. Hasteko erditxasi hau zein eratara fabrikatua izan daitekeen aztertuko da(hodi, txapa…), eta modu bakoitzaren abantailak eta desabantailak ikusi beharko dira azkenik nola egingo den aukeratzeko. Honela gure piezaren eboluzio bat emango da guk behar ditugun exijentzia teknikoak bete ditzan eta ekonomikoki ere bideragarria izan dadin. Amaitzeko pieza bere lekuan bermatzeko beharko diren elementu laguntzaileak ere kalkulatu edo aukeratu beharko dira, lehiaketan dugun portaera guk nahi duguna izan dadin.

Optical levitation measurements with intensity-modulated light beams

Illumination of an optically levitated particle with an intensity-modulated transverse beam induces a transverse vibration of a particle in an optical trap. Based on this, the trapping force of a trap can be measured. Using an intensity-modulated longitudinal levitating beam causes a particle to move vertically, allowing for the determination of some aerodynamic parameters of a particle in air. The principles and the experimental phenomena are described and the initial results are given. (C) 1997 Optical Society of America.

Methods for melting temperature calculation

Melting temperature calculation has important applications in the theoretical study of phase diagrams and computational materials screenings. In this thesis, we present two new methods, i.e., the improved Widom's particle insertion method and the small-cell coexistence method, which we developed in order to capture melting temperatures both accurately and quickly.

We propose a scheme that drastically improves the efficiency of Widom's particle insertion method by efficiently sampling cavities while calculating the integrals providing the chemical potentials of a physical system. This idea enables us to calculate chemical potentials of liquids directly from first-principles without the help of any reference system, which is necessary in the commonly used thermodynamic integration method. As an example, we apply our scheme, combined with the density functional formalism, to the calculation of the chemical potential of liquid copper. The calculated chemical potential is further used to locate the melting temperature. The calculated results closely agree with experiments.

We propose the small-cell coexistence method based on the statistical analysis of small-size coexistence MD simulations. It eliminates the risk of a metastable superheated solid in the fast-heating method, while also significantly reducing the computer cost relative to the traditional large-scale coexistence method. Using empirical potentials, we validate the method and systematically study the finite-size effect on the calculated melting points. The method converges to the exact result in the limit of a large system size. An accuracy within 100 K in melting temperature is usually achieved when the simulation contains more than 100 atoms. DFT examples of Tantalum, high-pressure Sodium, and ionic material NaCl are shown to demonstrate the accuracy and flexibility of the method in its practical applications. The method serves as a promising approach for large-scale automated material screening in which the melting temperature is a design criterion.

We present in detail two examples of refractory materials. First, we demonstrate how key material properties that provide guidance in the design of refractory materials can be accurately determined via ab initio thermodynamic calculations in conjunction with experimental techniques based on synchrotron X-ray diffraction and thermal analysis under laser-heated aerodynamic levitation. The properties considered include melting point, heat of fusion, heat capacity, thermal expansion coefficients, thermal stability, and sublattice disordering, as illustrated in a motivating example of lanthanum zirconate (La₂Zr₂O₇). The close agreement with experiment in the known but structurally complex compound La₂Zr₂O₇ provides good indication that the computation methods described can be used within a computational screening framework to identify novel refractory materials. Second, we report an extensive investigation into the melting temperatures of the Hf-C and Hf-Ta-C systems using ab initio calculations. With melting points above 4000 K, hafnium carbide (HfC) and tantalum carbide (TaC) are among the most refractory binary compounds known to date. Their mixture, with a general formula Ta_xHf_1-xC_y, is known to have a melting point of 4215 K at the composition Ta₄HfC₅, which has long been considered as the highest melting temperature for any solid. Very few measurements of melting point in tantalum and hafnium carbides have been documented, because of the obvious experimental difficulties at extreme temperatures. The investigation lets us identify three major chemical factors that contribute to the high melting temperatures. Based on these three factors, we propose and explore a new class of materials, which, according to our ab initio calculations, may possess even higher melting temperatures than Ta-Hf-C. This example also demonstrates the feasibility of materials screening and discovery via ab initio calculations for the optimization of "higher-level" properties whose determination requires extensive sampling of atomic configuration space.

Estudio del comportamiento aerodinámico de un alerón trasero de un monoplaza tipo Formula Student

[ES]El proyecto investigador tiene el objeto el estudio del comportamiento de un perfil aerodinámico frente a un flujo turbulento, en este caso el aire. Se trata de evaluar las presiones que se ejercen sobre dicho perfil, que será un alerón de monoplaza tipo Formula Student, para comprobar si aporta alguna mejora en el comportamiento del monoplaza la introducción de este paquete aerodinámico. Con la introducción de este perfil en el monoplaza se pretende ganar un mayor agarre en el paso por curva siendo la resistencia al avance en recta la mínima posible, ya que lo que se pretende es hacer el recorrido del circuito en el menor tiempo posible. Por tanto hay dos variables a tener en cuenta a la hora de diseñar el alerón, por un lado esta mejorar el agarre de los neumáticos sobre el asfalto al tomar una curva, lo que nos permitirá tomar la curva a mayor velocidad y por tanto en menos tiempo, y por otro lado, la oposición que el alerón ejerce en el avance en recta disminuyendo su velocidad máxima. En resumen, se trata de comparar la fuerza horizontal y la fuerza vertical que el aire ejerce sobre el perfil aerodinámico a introducir en el monoplaza y evaluar si es beneficioso para este, es decir, si añadiendo dicho perfil se realiza el trazado del circuito en menor tiempo que sin él. Para ello se realizarán simulaciones con un software de modelado físico de flujos y turbulencias sobre un diseño de un alerón dado, con diferentes tipos de flujo, de forma que se asemeje de mejor forma a las condiciones de la pista y se obtendrán los resultados de las presiones que el flujo de aire ejerce sobre las superficies del perfil. Después se obtendrán las fuerzas puntuales vertical y horizontal y se analizaran los datos obtenidos. Deberán tenerse en cuenta, además de los resultados obtenidos, los materiales a emplear a la hora de su fabricación, el proceso de dicha fabricación y el coste que supone tanto el proceso como los materiales empleados.

In Vitro Surfactant and Perfluorocarbon Aerosol Deposition in a Neonatal Physical Model of the Upper Conducting Airways

Objective: Aerosol delivery holds potential to release surfactant or perfluorocarbon (PFC) to the lungs of neonates with respiratory distress syndrome with minimal airway manipulation. Nevertheless, lung deposition in neonates tends to be very low due to extremely low lung volumes, narrow airways and high respiratory rates. In the present study, the feasibility of enhancing lung deposition by intracorporeal delivery of aerosols was investigated using a physical model of neonatal conducting airways. Methods: The main characteristics of the surfactant and PFC aerosols produced by a nebulization system, including the distal air pressure and air flow rate, liquid flow rate and mass median aerodynamic diameter (MMAD), were measured at different driving pressures (4-7 bar). Then, a three-dimensional model of the upper conducting airways of a neonate was manufactured by rapid prototyping and a deposition study was conducted. Results: The nebulization system produced relatively large amounts of aerosol ranging between 0.3 +/- 0.0 ml/min for surfactant at a driving pressure of 4 bar, and 2.0 +/- 0.1 ml/min for distilled water (H(2)Od) at 6 bar, with MMADs between 2.61 +/- 0.1 mu m for PFD at 7 bar and 10.18 +/- 0.4 mu m for FC-75 at 6 bar. The deposition study showed that for surfactant and H(2)Od aerosols, the highest percentage of the aerosolized mass (similar to 65%) was collected beyond the third generation of branching in the airway model. The use of this delivery system in combination with continuous positive airway pressure set at 5 cmH(2)O only increased total airway pressure by 1.59 cmH(2)O at the highest driving pressure (7 bar). Conclusion: This aerosol generating system has the potential to deliver relatively large amounts of surfactant and PFC beyond the third generation of branching in a neonatal airway model with minimal alteration of pre-set respiratory support.

Metodologia de projeto de turbinas eólicas de pequeno porte.

O potencial eólico do Brasil, de vento firme e com viabilidade econômica de aproveitamento, é de 143 GW. Isso equivale ao dobro de toda a capacidade da geração já instalada no país. No Brasil, a energia eólica tem uma sazonalidade complementar à energia hidrelétrica, porque os períodos de melhor condição de vento coincidem com os de menor capacidade dos reservatórios. O projeto desenvolvido neste trabalho nasceu de uma chamada pública do FINEP, e sob os auspícios do recém criado CEPER. Ao projeto foi incorporado um caráter investigativo, de contribuição científica original, resultando em um produto de tecnologia inovadora para aerogeradores de baixa potência. Dentre os objetivos do projeto, destacamos a avaliação experimental de turbinas eólicas de 5000 W de potência. Mais especificamente, dentro do objetivo geral deste projeto estão incluídas análise estrutural, análise aerodinâmica e análise de viabilidade de novos materiais a serem empregados. Para cada uma das diferentes áreas de conhecimento que compõem o projeto, será adotada a metodologia mais adequada. Para a Análise aerodinâmica foi realizada uma simulação numérica preliminar seguida de ensaios experimentais em túnel de vento. A descrição dos procedimentos adotados é apresentada no Capítulo 3. O Capítulo 4 é dedicado aos testes elétricos. Nesta etapa, foi desenvolvido um banco de testes para obtenção das características específicas das máquinas-base, como curvas de potência, rendimento elétrico, análise e perdas mecânicas e elétricas, e aquecimento. Este capítulo termina com a análise crítica dos valores obtidos. Foram realizados testes de campo de todo o conjunto montado. Atualmente, o aerogerador de 5kW encontra-se em operação, instrumentado e equipado com sistema de aquisição de dados para consolidação dos testes de confiabilidade. Os testes de campo estão ocorrendo na cidade de Campos, RJ, e abrangeram as seguintes dimensões de análise; testes de eficiência para determinação da curva de potência, níveis de ruído e atuação de dispositivos de segurança. Os resultados esperados pelo projeto foram atingidos, consolidando o projeto de um aerogerador de 5000W.

Apertem os cintos, o piloto sumiu: as escolhas profissionais juvenis no mundo contemporâneo

Esses escritos compõem as escolhas profissionais juvenis, desde a sua emergência no mundo moderno ao contemporâneo. Registrado, através de uma análise histórica em que os acontecimentos não são trazidos de forma linear, contínua e progressiva, mas em suas intensidades, lutas e surpresas. Um modo de pensar que afirmou as escolhas profissionais, afastando-as de sua força de afirmação da vida. Essas experimentações se tecem em uma pesquisa-intervenção na área da Orientação Vocacional, realizada no Serviço de Psicologia Aplicada da Universidade Federal Fluminense. Essa pesquisa acolhe o não saber escolher, para provocar tensões e torções, baseadas em leituras de autores da Filosofia da Diferença, da Psicologia, do Mundo do Trabalho. Assim, equivocar o modo de pensar predominante no Ocidente e abrir lacunas para que outros sentidos de inserção no mundo do trabalho se façam. Movimentar concepções estabelecidas, para fazê-las desconcertar e vibrar, acolhendo o ainda não sentido. Poder surpreender e inventar outros modos de se conduzir frente às escolhas profissionais, no enfrentamento dos impasses que o contemporâneo apresenta.

Condições de contorno tipo albedo para cálculos globais de reatores nucleares com o modelo de dois grupos de energia na formulação de transporte SN em geometria bidimensional cartesiana

Os eventos de fissão nuclear, resultados da interação dos nêutrons com os núcleos dos átomos do meio hospedeiro multiplicativo, não estão presentes em algumas regiões dos reatores nucleares, e.g., moderador, refletor, e meios estruturais. Nesses domínios espaciais não há geração de potência nuclear térmica e, além disso, comprometem a eficiência computacional dos cálculos globais de reatores nucleares. Propomos nesta tese uma estratégia visando a aumentar a eficiência computacional dessas simulações eliminando os cálculos numéricos explícitos no interior das regiões não-multiplicativas (baffle e refletor) em torno do núcleo ativo. Apresentamos algumas modelagens e discutimos a eficiência da aplicação dessas condições de contorno aproximadas tipo albedo para uma e duas regiões nãomultiplicativas, na formulação de ordenadas discretas (SN) para problemas de autovalor a dois grupos de energia em geometria bidimensional cartesiana. A denominação Albedo, palavra de origem latina para alvura, foi originalmente definida como a fração da luz incidente que é refletida difusamente por uma superfície. Esta denominação latina permaneceu como o termo científico usual em astronomia e, nesta tese, este conceito é estendido para reflexão de nêutrons. Estas condições de contorno tipo albedo SN não-convencional substituem aproximadamente as regiões de baffle e refletor no em torno do núcleo ativo do reator, desprezando os termos de fuga transversal no interior dessas regiões. Se o problema, em particular, não possui termos de fuga transversal, i.e., trata-se de um problema unidimensional, então as condições de contorno albedo, como propostas nesta tese, são exatas. Por eficiência computacional entende-se a análise da precisão dos resultados numéricos em comparação com o tempo de execução computacional de cada simulação de um dado problema-modelo. Resultados numéricos considerando dois problemas-modelo com de simetria são considerados para ilustrar esta análise de eficiência.

Landing gear for a 'silent' aircraft

The Silent Aircraft Initiative aims to provide a conceptual design for a large passenger aircraft whose noise would be imperceptible above the background level outside an urban airfield. Landing gear noise presents a significant challenge to such an aircraft. 1/10th scale models have been examined with the aim of establishing a lower noise limit for large aircraft landing gear. Additionally, the landing gear has been included in an integrated design concept for the 'Silent' Aircraft. This work demonstrates the capabilities of the closed-section Markham wind tunnel and the installed phased microphone arrays for aerodynamic and acoustic measurements. Interpretation of acoustic data has been enhanced by use of the CLEAN algorithm to quantify noise levels in a repeatable way and to eliminate side lobes which result from the microphone array geometry. Results suggest that highly simplified landing gears containing only the main struts offer a 12dBA reduction from modern gear noise. Noise treatment of simplified landing gear with fairings offers a further reduction which appears to be limited by noise from the lower parts of the wheels. The importance of fine details and surface discontinuities for low noise design are also underlined.

The effects of docks on seagrasses, with particular emphasis on the threatened seagrass, Halophila johnsonii

In March of 2005, the National Oceanic and Atmospheric Administration's Special Projects Office released "Population Trends along the Coastal United States: 1980-2008." This report includes population changes and trends between 1980 and 2003 and projected changes in coastal populations by 2008. Given the findings, pressure on coastal resources around the country will continue to rise, particularly in Florida. ... One of our most valuable coastal resources is seagrass, but human desire and need to live on the coast means that our habitat overlaps with suitable seagrass habitat. Seagrasses can be found in coastal areas around the world but are limited to relatively shallow, relatively clear water because of their reliance on light for photosynthesis. Seagrasses provide food for both small and large marine organisms, larval and adult stage. They provide shelter and habitat to a variety of commercially important fish and invertebrates. They baffle the water column and inhibit the resuspension of sediments. They prevent erosion and fix and recycle nutrients. The physical and ecological benefits of seagrasses make them very important to human welfare, but their light-limited coastal distribution makes them highly susceptible to anthropogenic influences.

Articulated wooden blades for a horizontal-axis wind turbine. Design, construction and testing.

A pair of blades were constructed following a Tapered Chord, Zero Twist pattern after Anderson. The construction uses the Wood Epoxy Saturation Technique, with a solid Beech main spar and leading edge joined together with laminated veneers of beech forming a D-section; the trailing edge is formed from millimetre ply skins, foam filled to resist compressive loads. This construction leads to an extremely light, flexible blade, with the centres of gravity and torsion well forward, giving good stability. Each blade has three built-in strain gauges, alowing flapwise bending to be measured. Stiffness, and natural frequencies, were measured, to input to a numerical computer model to calculate blade deformation during operation, and to determine stability boundaries of the blade. Preliminary aerodynamic performance measurements are presented and close agreement is found with theory.