Aufbau und Charakterisierung eines flugzeuggetragenen Einzelpartikel-Massenspektrometers

Im Rahmen dieser Arbeit wurde ein flugzeuggetragenes Laserablations-Einzelpartikel-Massenspektrometer von Grund auf entworfen, gebaut, charakterisiert und auf verschiedenen Feldmesskampagnen eingesetzt. Das ALABAMA (Aircraft-based Laser ABlation Aerosol MAss Spectrometer) ist in der Lage die chemische Zusammensetzung und Größe von einzelnen Aerosolpartikeln im submikrometer-Bereich (135 – 900 nm) zu untersuchen.rnNach dem Fokussieren in einer aerodynamischen Linse wird dafür zunächst derrnaerodynamische Durchmesser der einzelnen Partikel mit Hilfe einer Flugzeitmessung zwischen zwei Dauerstrichlasern bestimmt. Anschließend werden die zuvor detektierten und klassifizierten Partikel durch einen gezielten Laserpuls einzeln verdampft und ionisiert. Die Ionen werden in einem bipolaren Flugzeit-Massenspektrometer entsprechend ihrem Masse zu- Ladungs Verhältnisses getrennt und detektiert. Die entstehenden Massenspektren bieten einen detaillierten Einblick in die chemische Struktur der einzelnen Partikel.rnDas gesamte Instrument wurde so konzipiert, dass es auf dem neuen Höhenforschungsflugzeug HALO und anderen mobilen Plattformen eingesetzt werden kann. Um dies zu ermöglichen wurden alle Komponenten in einem Rahmen mit weniger als 0.45 m³ Volumen untergebracht. Das gesamte Instrument inklusive Rahmen wiegt weniger als 150 kg und erfüllt die strengen sicherheitsvorschriften für den Betrieb an Bord von Forschungsflugzeugen. Damit ist ALABAMA das kleinste und leichteste Instrument seiner Art.rnNach dem Aufbau wurden die Eigenschaften und Grenzen aller Komponenten detailliert im Labor und auf Messkampagnen charakterisiert. Dafür wurden zunächst die Eigenschaften des Partikelstrahls, wie beispielsweise Strahlbreite und –divergenz, ausführlich untersucht. Die Ergebnisse waren wichtig, um die späteren Messungen der Detektions- und Ablationseffizienz zu validieren.rnBei den anschließenden Effizienzmessungen wurde gezeigt, dass abhängig von ihrer Größe und Beschaffenheit, bis zu 86 % der vorhandenen Aerosolpartikel erfolgreich detektiert und größenklassifiziert werden. Bis zu 99.5 % der detektierten Partikel konnten ionisiert und somit chemisch untersucht werden. Diese sehr hohen Effizienzen sind insbesondere für Messungen in großer Höhe entscheidend, da dort zum Teil nur sehr geringe Partikelkonzentrationen vorliegen.rnDas bipolare Massenspektrometer erzielt durchschnittliche Massenauflösungen von bis zu R=331. Während Labor- und Feldmessungen konnten dadurch Elemente wie Au, Rb, Co, Ni, Si, Ti und Pb eindeutig anhand ihres Isotopenmusters zugeordnet werden.rnErste Messungen an Bord eines ATR-42 Forschungsflugzeuges während der MEGAPOLI Kampagne in Paris ergaben einen umfassenden Datensatz von Aerosolpartikeln innerhalb der planetaren Grenzschicht. Das ALABAMA konnte unter harten physischen Bedingungen (Temperaturen > 40°C, Beschleunigungen +/- 2 g) verlässlich und präzise betrieben werden. Anhand von charakteristischen Signalen in den Massenspektren konnten die Partikel zuverlässig in 8 chemische Klassen unterteilt werden. Einzelne Klassen konnten dabei bestimmten Quellen zugeordnet werden. So ließen sich beispielsweise Partikel mit starkerrnNatrium- und Kaliumsignatur eindeutig auf die Verbrennung von Biomasse zurückführen.rnALABAMA ist damit ein wertvolles Instrument um Partikel in-situ zu charakterisieren und somit verschiedenste wissenschaftliche Fragestellungen, insbesondere im Bereich der Atmosphärenforschung, zu untersuchen.

Untersuchung der Adhäsionskräfte in interaktiven Pulvermischungen zur Inhalation und deren Veränderung in Abhängigkeit von der Dichtigkeit der Verpackung

Die Untersuchung der Adhäsionskräfte mit Colloid Probe Technik, einer Weiterentwicklung der Rasterkraftmikroskopie (Atomic Force Microscopy=AFM), an erzeugten Carrier- und Wirkstoffkristallen bei Laborbedingungen und unter Einfluss der Luftfeuchte zeigte, dass die Adhäsion von Tiotropiumbromid Monohydrat an Mannitol deutlich höher ist als an Lactose Monohydrat. Die Kohäsionskräfte des Wirkstoffes sind stärker als die Adhäsionskräfte an Carriermaterialien. Auf dieser Grundlage wurde die Hypothese aufgestellt, dass eine Mischung mit Mannitol als Carrier eine kleinere Feinpartikeldosis liefert als eine Mischung mit Lactose. Diese Theorie wurde an interaktiven Pulvermischungen unter Variation von verschiedenen Einflussfaktoren überprüft. Die binare und ternäre Lactose-basierte Mischung lieferte unabhängig vom Kapselmaterial (Gelatine- und Polyethylenkapsel) eine höhere Feinpartikeldosis als die entsprechenden Mannitol-basierten Formulierungen. Die ternäre Komponente bewirkte nur bei Mannitol-basierten Mischungen eine Verbesserung der Feinpartikeldosis. Die detaillierte Untersuchung der aerodynamischen Verteilung ternärer Mischungen zeigte, dass das Kapselmaterial nur unter dem Einfluss der Luftfeuchte und Permeabilität der Blisterverpackung die interpartikulären Wechselwirkungen beeinflusst. Mischungen mit Mannitol als Carrier lieferten unabhängig vom Kapselmaterial, von Luftfeuchte/Lagerungsbedingungen und Permeabilität der Blisterverpackung eine kleinere Feinpartikeldosis als Mischungen mit Lactose als Carrier. Die Carrierart, die Permeabilität der Blisterverpackung und die Luftfeuchte wurden als Haupteinflussfaktoren auf die aerodynamischen Eigenschaften identifiziert. Es konnte gezeigt werden, dass AFM einen wertvollen Beitrag zum Verständnis der interpartikulären Wechselwirkungen leistet und aufgrund prädiktiver Eigenschaften hilfreich in der Entwicklung inhalativer Darreichungs-formen sein kann.

Aereodynamics of dry helically-filleted bridge cables

Dry limited amplitude vibrations flow-transition induced vibrations were experienced on a helically-filleted tube, in a previous study performed by Kleissl and Georgakis (2012). These vibrations have never been reported in previous studies. A deep study on the same inclined-yawed cable configuration has been performed, in order to investigate and further understand the nature of these vibrations. The investigation has been carried out through passive-dynamic wind tunnel tests in the Climatic Wind Tunnel at FORCE Technology, Kgs. Lyngby, Denmark. The results are carried out in terms of aerodynamic damping and peak to peak amplitude at different flow velocities and different boundary conditions. The latter are done by testing the model with and without the spray system installed in the wind tunnel cross section, in order to understand and evaluate the influence of the spray system on the start of the vibrations mechanism and on the flow turbulence. The gained experiences are finally presented for the use in future testing activities with the purpose of improving the performance of passive-dynamic tests.

Aeroelastic stability of structures: flutter analysis using Computational Fluid Dynamics

Thanks to the increasing slenderness and lightness allowed by new construction techniques and materials, the effects of wind on structures became in the last decades a research field of great importance in Civil Engineering. Thanks to the advances in computers power, the numerical simulation of wind tunnel tests has became a valid complementary activity and an attractive alternative for the future. Due to its flexibility, during the last years, the computational approach gained importance with respect to the traditional experimental investigation. However, still today, the computational approach to fluid-structure interaction problems is not as widely adopted as it could be expected. The main reason for this lies in the difficulties encountered in the numerical simulation of the turbulent, unsteady flow conditions generally encountered around bluff bodies. This thesis aims at providing a guide to the numerical simulation of bridge deck aerodynamic and aeroelastic behaviour describing in detail the simulation strategies and setting guidelines useful for the interpretation of the results.

Optimierung der inhalativen Therapie bei Patienten mit Cystischer Fibrose und bei Kleinkindern

Patienten mit Cystischer Fibrose müssen in der Regel verschiedene Arzneimittel mehrmals täglich inhalieren. Um den hohen Zeitaufwand dafür zu reduzieren werden die Arzneimittel häufig gemischt und simultan inhaliert. Die Kenntnis der physikalisch-chemischen Kompatibilität von Mischinhalationslösungen/ -suspensionen ist deshalb von großer Bedeutung. In der vorliegenden Arbeit wurden die Kompatibilitäten von Mischungen aus Colistimethat-Inhalationslösung (mikrobiologische Wertbestimmung) mit verschiedenen Tobramycin-Inhalationslösungen, Budesonid (HPLC) mit 5,85%-iger Natriumchlorid-Lösung sowie mit Colistimethat-Inhalationslösung und Dornase alfa (SE-HPLC, SDS-PAGE, UV-Spektrometrie, T-SCX-Chromatographie) mit verschiedenen Tobramycin-Inhalationslösungen (Fluoreszenzpolarisations-Immunoassay) nachgewiesen. Durch das Mischen mit Tobramycin-Inhalationslösungen wurden die aerodynamischen Eigenschaften (FPF, MMAD, GSD) von Dornase alfa bei simultaner Verneblung nicht verändert (bestimmt mittels Kaskadenimpaktion).rnDurch die physiologischen und anatomischen Gegebenheiten, sowie die kognitiven Fähigkeiten kleiner Kinder stellt die effektive inhalative Therapie eine große Herausforderung dar. Der Respimat® bietet mit seiner langen Sprühdauer und den kleinen Aerosolpartikeln eine vielversprechende Alternative für die Anwendung bei Kleinkindern. In der vorliegenden Studie wurde untersucht ob bei Kindern unter 5 Jahren der Respimat® als Inhalationsgerät verwendet werden kann und welchen Grad an Hilfestellung sie für ein erfolgreiches Inhalationsmanöver benötigen.rnDie Ergebnisse der Handhabungsuntersuchung, sowie die Bewertung aufgezeichneter Inhalationsprofile zeigten, dass der Respimat® für Kinder < 4 Jahre nur in Kombination mit einer Inhalierhilfe wie dem AeroChamber Plus® verwendet werden sollte. Kinder im Alter von 4 Jahren sind mit entsprechender Schulung in der Lage mit dem Respimat® alleine zu inhalieren.rn

Fault detection, diagnosis and active fault tolerant control for a satellite attitude control system

Modern control systems are becoming more and more complex and control algorithms more and more sophisticated. Consequently, Fault Detection and Diagnosis (FDD) and Fault Tolerant Control (FTC) have gained central importance over the past decades, due to the increasing requirements of availability, cost efficiency, reliability and operating safety. This thesis deals with the FDD and FTC problems in a spacecraft Attitude Determination and Control System (ADCS). Firstly, the detailed nonlinear models of the spacecraft attitude dynamics and kinematics are described, along with the dynamic models of the actuators and main external disturbance sources. The considered ADCS is composed of an array of four redundant reaction wheels. A set of sensors provides satellite angular velocity, attitude and flywheel spin rate information. Then, general overviews of the Fault Detection and Isolation (FDI), Fault Estimation (FE) and Fault Tolerant Control (FTC) problems are presented, and the design and implementation of a novel diagnosis system is described. The system consists of a FDI module composed of properly organized model-based residual filters, exploiting the available input and output information for the detection and localization of an occurred fault. A proper fault mapping procedure and the nonlinear geometric approach are exploited to design residual filters explicitly decoupled from the external aerodynamic disturbance and sensitive to specific sets of faults. The subsequent use of suitable adaptive FE algorithms, based on the exploitation of radial basis function neural networks, allows to obtain accurate fault estimations. Finally, this estimation is actively exploited in a FTC scheme to achieve a suitable fault accommodation and guarantee the desired control performances. A standard sliding mode controller is implemented for attitude stabilization and control. Several simulation results are given to highlight the performances of the overall designed system in case of different types of faults affecting the ADCS actuators and sensors.

Contributo sperimentale alla ridefinizione della diffusione in parete della camera di prova della galleria del vento Dallara

Joseph Nicolas Cugnot built the first primitive car in 1769 and approximately one hundred year later the first automotive race took place. Thanks to this, for the first time the aerodynamics principles began to be applied to cars. The aerodynamic study of a car is important to improve the performance on the road, or on the track. It purposely enhances the stability in the turns and increases the maximum velocity. However, it is also useful, decrease the fuel consumption, in order to reduce the pollution. Given that cars are a very complex body, the aerodynamic study cannot be conducted following an analytical method, but it is possible, in general, to choose between two different approaches: the numerical or the experimental one. The results of numerical studies depend on the computers’ potential and on the method use to implement the mathematical model. Today, the best way to perform an aerodynamic study is still experimental, which means that in the first phase of the design process the study is performed in a wind tunnel and in later phases directly on track. The automotive wind tunnels are singular mainly due to the test chamber, which typically contains a ground simulation system. The test chamber can have different types of walls: open walls, closed walls, adaptive walls or slotted walls. The best solution is to use the slotted walls because they minimize the interference between the walls and the streamlines, the interaction between the flow and the environment, and also to contain the overall costs. Furthermore, is necessary minimize the boundary layer at the walls, without accelerating the flow, in order to provide the maximum section of homogeneous flow. This thesis aims at redefining the divergent angle of the Dallara Automobili S.P.A. wind tunnel’s walls, in order to improve the overall homogeneity. To perform this study it was necessary to acquire the pressure data of the boundary layer, than it was created the profile of the boundary layer velocity and, to minimize the experimental errors, it was calculated the displacement thickness. The results obtained shows, even if the instrument used to the experiment was not the best one, that the boundary layer thickness could be minor in case of a low diffusion angle. So it is convenient to perform another experiment with a most sensitive instrument to verified what is the better wall configuration.

Dynamics and control issues of multi-rotor platforms

This thesis deals with the analytic study of dynamics of Multi--Rotor Unmanned Aerial Vehicles. It is conceived to give a set of mathematical instruments apt to the theoretical study and design of these flying machines. The entire work is organized in analogy with classical academic texts about airplane flight dynamics. First, the non--linear equations of motion are defined and all the external actions are modeled, with particular attention to rotors aerodynamics. All the equations are provided in a form, and with personal expedients, to be directly exploitable in a simulation environment. This has requited an answer to questions like the trim of such mathematical systems. All the treatment is developed aiming at the description of different multi--rotor configurations. Then, the linearized equations of motion are derived. The computation of the stability and control derivatives of the linear model is carried out. The study of static and dynamic stability characteristics is, thus, addressed, showing the influence of the various geometric and aerodynamic parameters of the machine and in particular of the rotors. All the theoretic results are finally utilized in two interesting cases. One concerns the design of control systems for attitude stabilization. The linear model permits the tuning of linear controllers gains and the non--linear model allows the numerical testing. The other case is the study of the performances of an innovative configuration of quad--rotor aircraft. With the non--linear model the feasibility of maneuvers impossible for a traditional quad--rotor is assessed. The linear model is applied to the controllability analysis of such an aircraft in case of actuator block.

Einsatz eines Aerosolmassenspektrometers während der CYPHEX-Kampagne und zur Methodenentwicklung einer Echtzeitquantifizierung gasförmiger Amine

Atmosphärische Aerosole haben einen starken Einfluss auf das Klima, der bisher nur grundlegend verstanden ist und weiterer Forschung bedarf. Das atmosphärische Verhalten der Aerosolpartikel hängt maßgeblich von ihrer Größe und chemischen Zusammensetzung ab. Durch Reflexion, Absorption und Streuung des Sonnenlichtes verändern sie den Strahlungshaushalt der Erde direkt und durch ihre Einflussnahme auf die Wolkenbildung indirekt. Besonders gealterte, stark oxidierte organische Aerosole mit großem Sauerstoff-zu-Kohlenstoff-Verhältnis wirken als effektive Wolkenkondensationskeime. Neben primären Aerosolpartikeln, die direkt partikelförmig in die Atmosphäre gelangen, spielen sekundäre Aerosolpartikel eine große Rolle, die aus Vorläufergasen in der Atmosphäre entstehen. Aktuelle Forschungsergebnisse legen nahe, dass kurzkettige aliphatische Amine bei Nukleationsprozessen beteiligt sind und somit die Partikelneubildung vielerorts mitsteuern. Um die Rolle von Aminen in der Atmosphäre besser erforschen und industrielle Emissionen kontrollieren zu können, bedarf es einer zuverlässigen Methode zur Echtzeitquantifizierung gasförmiger Amine mit hoher Zeitauflösung und niedriger Nachweisgrenze.rnDas hochauflösende Flugzeit-Aerosolmassenspektrometer (HR-ToF-AMS) bietet die Möglichkeit, atmosphärische Partikel in Echtzeit zu analysieren. Dabei werden Größe, Menge und grundlegende chemische Zusammensetzung erfasst. Anorganische Aerosolbestandteile können eindeutig zugeordnet werden. Es ist jedoch kaum möglich, einzelne organische Verbindungen in den komplizierten Massenspektren atmosphärischer Aerosole zu identifizieren und quantifizieren.rnIn dieser Arbeit wird atmosphärisches Aerosol untersucht, das im Westen Zyperns während der CYPHEX-Kampagne mit einem HR-ToF-AMS gemessen wurde. An diesem Standort ist vor allem stark gealtertes Aerosol vorzufinden, das aus Zentral- und Westeuropa stammt. Lokale Einflüsse spielen fast keine Rolle. Es wurde eine durchschnittliche Massenkonzentration von 10,98 μg/m3 gefunden, zusammengesetzt aus 57 % Sulfat, 30 % organischen Bestandteilen, 12 % Ammonium, < 1 % Nitrat und < 1 % Chlorid, bezogen auf das Gewicht. Der Median des vakuum-aerodynamischen Durchmessers betrug 446,25 nm. Es wurde sehr acides Aerosol gefunden, dessen anorganische Bestandteile weitgehend der Zusammensetzung von Ammoniumhydrogensulfat entsprachen. Tag-Nacht-Schwankungen in der Zusammensetzung wurden beobachtet. Die Sulfatkonzentration und die Acidität zeigten tagsüber Maxima und nachts Minima. Konzentrationsschwankungen an Nitrat und Chlorid zeigten einen weniger ausgeprägten Rhythmus, Maxima fallen aber immer mit Minima der Sulfatkonzentration, Aerosolacidität und Umgebungstemperatur zusammen. Organische Aerosolbestandteile entsprachen stark gealtertem, schwerflüchtigem oxidiertem organischem Aerosol. Es wurde eine interne Mischung der Partikel beobachtet, die ebenfalls meist bei alten Aerosolen auftritt.rnUm mit dem HR-ToF-AMS auch einzelne organische Verbindungen identifizieren und quantifizieren zu können, wurde eine Methode entwickelt, mit der man Amine der Gasphase selektiv in künstlich erzeugte Phosphorsäurepartikel aufnimmt und so für die HR-ToF-AMS-Messung zugänglich macht. Dadurch kombiniert man die Vorteile der Online-Messung des HR-ToF-AMS mit den Vorteilen klassischer Offline-Probenahmen. So können in Echtzeit sehr einfache Massenspektren gemessen werden, in denen störende Komponenten abgetrennt sind, während die Analyten eindeutig identifiziert werden können. Systeme dieser Art wurden GTRAP-AMS (Gaseous compound TRapping in Artificially-generated Particles – Aerosol Mass Spectrometry) genannt. Kalibrierungen für (Mono)Methylamin, Dimethylamin, Trimethylamin, Diethylamin und Triethylamin ergaben Nachweisgrenzen im ppt-Bereich bei einer Zeitauflösung von 3 min. Kammerexperimente zur Aminemission von Pflanzen zeigten eine gute Übereinstimmung des neu entwickelten Systems mit einer Gasdiffusionsabscheider-Offline-Probenahme und anschließender ionenchromatographischer Analyse. Beide Methoden zeigten Reaktionen der Pflanzen auf eine Veränderung der Lichtverhältnisse, während erhöhte Ozonkonzentrationen die Aminemission nicht veränderten. Die GTRAP-AMS-Methode eignet sich bereits für die Messung von Umgebungsluftkonzentrationen an einigen Orten, für die meisten Orte reicht die Nachweisgrenze allerdings noch nicht aus. Die Technik könnte bereits zur Echtzeitkontrolle industrieller Abgasemissionen eingesetzt werden.

Characterization of Halyomorpha Halys (Brown Marmorated Stink Bug) Biogenic Volatile Organic Compound Emissions and Their Role in Secondary Organic Aerosol Formation

The formation of aerosols is a key component in understanding cloud formation in the context of radiative forcings and global climate modeling. Biogenic volatile organic compounds (BVOCs) are a significant source of aerosols, yet there is still much to be learned about their structures, sources, and interactions. The aims of this project were to identify the BVOCs found in the defense chemicals of the brown marmorated stink bug Halymorpha halys and quantify them using gas chromatography-mass spectrometry (GC/MS) and test whether oxidation of these compounds by ozone-promoted aerosol and cloud seed formation. The bugs were tested under two conditions: agitation by asphyxiation and direct glandular exposure. Tridecane, 2(5H)-furanone 5-ethyl, and (E)-2-decenal were identified as the three most abundant compounds. H. halys were also tested in the agitated condition in a smog chamber. It was found that in the presence of 100-180 ppm ozone, secondary aerosols do form. A scanning mobility particle sizer (SMPS) and a cloud condensation nuclei counter (CCNC) were used to characterize the secondary aerosols that formed. This reaction resulted in 0.23 mu g/bug of particulate mass. It was also found that these secondary organic aerosol particles could act as cloud condensation nuclei. At a supersaturation of 1%, we found a kappa value of 0.09. Once regional populations of these stink bugs stablilize and the populations estimates can be made, the additional impacts of their contribution to regional air quality can be calculated. Implications: Halymorpha halys (brown marmorated stink bugs) are a relatively new invasive species introduced in the United States near Allentown, Pennsylvania. The authors chemically speciated the bugs' defense pheromones and found that tridecane, 5-ethyl-2(5H)-furanone, and (E)-2-decenal dominated their emissions. Their defense emissions were reacted with atmospherically relevant concentrations of ozone and resulted in 0.23 g of particulate matter per emission per bug. Due to the large population of these bugs in some regions, these emissions could contribute appreciably to a region's PM2.5 (particulate matter with an aerodynamic diameter 2.5 m) levels.

Exposure to moderate air pollution during late pregnancy and cord blood cytokine secretion in healthy neonates

Background/Objectives Ambient air pollution can alter cytokine concentrations as shown in vitro and following short-term exposure to high air pollution levels in vivo. Exposure to pollution during late pregnancy has been shown to affect fetal lymphocytic immunophenotypes. However, effects of prenatal exposure to moderate levels of air pollutants on cytokine regulation in cord blood of healthy infants are unknown. Methods In a birth cohort of 265 healthy term-born neonates, we assessed maternal exposure to particles with an aerodynamic diameter of 10 µm or less (PM10), as well as to indoor air pollution during the last trimester, specifically the last 21, 14, 7, 3 and 1 days of pregnancy. As a proxy for traffic-related air pollution, we determined the distance of mothers' homes to major roads. We measured cytokine and chemokine levels (MCP-1, IL-6, IL-10, IL-1ß, TNF-α and GM-CSF) in cord blood serum using LUMINEX technology. Their association with pollution levels was assessed using regression analysis, adjusted for possible confounders. Results Mean (95%-CI) PM10 exposure for the last 7 days of pregnancy was 18.3 (10.3–38.4 µg/m3). PM10 exposure during the last 3 days of pregnancy was significantly associated with reduced IL-10 and during the last 3 months of pregnancy with increased IL-1ß levels in cord blood after adjustment for relevant confounders. Maternal smoking was associated with reduced IL-6 levels. For the other cytokines no association was found. Conclusions Our results suggest that even naturally occurring prenatal exposure to moderate amounts of indoor and outdoor air pollution may lead to changes in cord blood cytokine levels in a population based cohort.

MORTALITY IN THE MEDICARE POPULATION AND CHRONIC EXPOSURE TO FINE PARTICULATE AIR POLLUTION

Prospective cohort studies have provided evidence on longer-term mortality risks of fine particulate matter (PM2.5), but due to their complexity and costs, only a few have been conducted. By linking monitoring data to the U.S. Medicare system by county of residence, we developed a retrospective cohort study, the Medicare Air Pollution Cohort Study (MCAPS), comprising over 20 million enrollees in the 250 largest counties during 2000-2002. We estimated log-linear regression models having as outcome the age-specific mortality rate for each county and as the main predictor, the average level for the study period 2000. Area-level covariates were used to adjust for socio-economic status and smoking. We reported results under several degrees of adjustment for spatial confounding and with stratification into by eastern, central and western counties. We estimated that a 10 µg/m3 increase in PM25 is associated with a 7.6% increase in mortality (95% CI: 4.4 to 10.8%). We found a stronger association in the eastern counties than nationally, with no evidence of an association in western counties. When adjusted for spatial confounding, the estimated log-relative risks drop by 50%. We demonstrated the feasibility of using Medicare data to establish cohorts for follow-up for effects of air pollution. Particulate matter (PM) air pollution is a global public health problem (1). In developing countries, levels of airborne particles still reach concentrations at which serious health consequences are well-documented; in developed countries, recent epidemiologic evidence shows continued adverse effects, even though particle levels have declined in the last two decades (2-6). Increased mortality associated with higher levels of PM air pollution has been of particular concern, giving an imperative for stronger protective regulations (7). Evidence on PM and health comes from studies of acute and chronic adverse effects (6). The London Fog of 1952 provides dramatic evidence of the unacceptable short-term risk of extremely high levels of PM air pollution (8-10); multi-site time-series studies of daily mortality show that far lower levels of particles are still associated with short-term risk (5)(11-13). Cohort studies provide complementary evidence on the longer-term risks of PM air pollution, indicating the extent to which exposure reduces life expectancy. The design of these studies involves follow-up of cohorts for mortality over periods of years to decades and an assessment of mortality risk in association with estimated long-term exposure to air pollution (2-4;14-17). Because of the complexity and costs of such studies, only a small number have been conducted. The most rigorously executed, including the Harvard Six Cities Study and the American Cancer Society’s (ACS) Cancer Prevention Study II, have provided generally consistent evidence for an association of long- term exposure to particulate matter air pollution with increased all-cause and cardio-respiratory mortality (2,4,14,15). Results from these studies have been used in risk assessments conducted for setting the U.S. National Ambient Air Quality Standard (NAAQS) for PM and for estimating the global burden of disease attributable to air pollution (18,19). Additional prospective cohort studies are necessary, however, to confirm associations between long-term exposure to PM and mortality, to broaden the populations studied, and to refine estimates by regions across which particle composition varies. Toward this end, we have used data from the U.S. Medicare system, which covers nearly all persons 65 years of age and older in the United States. We linked Medicare mortality data to (particulate matter less than 2.5 µm in aerodynamic diameter) air pollution monitoring data to create a new retrospective cohort study, the Medicare Air Pollution Cohort Study (MCAPS), consisting of 20 million persons from 250 counties and representing about 50% of the US population of elderly living in urban settings. In this paper, we report on the relationship between longer-term exposure to PM2.5 and mortality risk over the period 2000 to 2002 in the MCAPS.

Air pollution during pregnancy and lung function in newborns: a birth cohort study

Post-natal exposure to air pollution is associated with diminished lung growth during school age. The current authors aimed to determine whether pre-natal exposure to air pollution is associated with lung function changes in the newborn. In a prospective birth cohort of 241 healthy term-born neonates, tidal breathing, lung volume, ventilation inhomogeneity and exhaled nitric oxide (eNO) were measured during unsedated sleep at age 5 weeks. Maternal exposure to particles with a 50% cut-off aerodynamic diameter of 10 microm (PM(10)), nitrogen dioxide (NO(2)) and ozone (O(3)), and distance to major roads were estimated during pregnancy. The association between these exposures and lung function was assessed using linear regression. Minute ventilation was higher in infants with higher pre-natal PM(10) exposure (24.9 mL x min(-1) per microg x m(-3) PM(10)). The eNO was increased in infants with higher pre-natal NO(2) exposure (0.98 ppb per microg x m(-3) NO(2)). Post-natal exposure to air pollution did not modify these findings. No association was found for pre-natal exposure to O(3) and lung function parameters. The present results suggest that pre-natal exposure to air pollution might be associated with higher respiratory need and airway inflammation in newborns. Such alterations during early lung development may be important regarding long-term respiratory morbidity.

Dynamic modeling, simulation and control design of a parafoil-payload system for ship launched aerial delivery system (SLADS)

The objective of this research was to develop a high-fidelity dynamic model of a parafoilpayload system with respect to its application for the Ship Launched Aerial Delivery System (SLADS). SLADS is a concept in which cargo can be transfered from ship to shore using a parafoil-payload system. It is accomplished in two phases: An initial towing phase when the glider follows the towing vessel in a passive lift mode and an autonomous gliding phase when the system is guided to the desired point. While many previous researchers have analyzed the parafoil-payload system when it is released from another airborne vehicle, limited work has been done in the area of towing up the system from ground or sea. One of the main contributions of this research was the development of a nonlinear dynamic model of a towed parafoil-payload system. After performing an extensive literature review of the existing methods of modeling a parafoil-payload system, a five degree-of-freedom model was developed. The inertial and geometric properties of the system were investigated to predict accurate results in the simulation environment. Since extensive research has been done in determining the aerodynamic characteristics of a paraglider, an existing aerodynamic model was chosen to incorporate the effects of air flow around the flexible paraglider wing. During the towing phase, it is essential that the parafoil-payload system follow the line of the towing vessel path to prevent an unstable flight condition called ‘lockout’. A detailed study of the causes of lockout, its mathematical representation and the flight conditions and the parameters related to lockout, constitute another contribution of this work. A linearized model of the parafoil-payload system was developed and used to analyze the stability of the system about equilibrium conditions. The relationship between the control surface inputs and the stability was investigated. In addition to stability of flight, one more important objective of SLADS is to tow up the parafoil-payload system as fast as possible. The tension in the tow cable is directly proportional to the rate of ascent of the parafoil-payload system. Lockout instability is more favorable when tow tensions are large. Thus there is a tradeoff between susceptibility to lockout and rapid deployment. Control strategies were also developed for optimal tow up and to maintain stability in the event of disturbances.

Structural response and dynamics of fluid-structure-control interaction in wind turbine blades

Reducing the uncertainties related to blade dynamics by the improvement of the quality of numerical simulations of the fluid structure interaction process is a key for a breakthrough in wind-turbine technology. A fundamental step in that direction is the implementation of aeroelastic models capable of capturing the complex features of innovative prototype blades, so they can be tested at realistic full-scale conditions with a reasonable computational cost. We make use of a code based on a combination of two advanced numerical models implemented in a parallel HPC supercomputer platform: First, a model of the structural response of heterogeneous composite blades, based on a variation of the dimensional reduction technique proposed by Hodges and Yu. This technique has the capacity of reducing the geometrical complexity of the blade section into a stiffness matrix for an equivalent beam. The reduced 1-D strain energy is equivalent to the actual 3-D strain energy in an asymptotic sense, allowing accurate modeling of the blade structure as a 1-D finite-element problem. This substantially reduces the computational effort required to model the structural dynamics at each time step. Second, a novel aerodynamic model based on an advanced implementation of the BEM(Blade ElementMomentum) Theory; where all velocities and forces are re-projected through orthogonal matrices into the instantaneous deformed configuration to fully include the effects of large displacements and rotation of the airfoil sections into the computation of aerodynamic forces. This allows the aerodynamic model to take into account the effects of the complex flexo-torsional deformation that can be captured by the more sophisticated structural model mentioned above. In this thesis we have successfully developed a powerful computational tool for the aeroelastic analysis of wind-turbine blades. Due to the particular features mentioned above in terms of a full representation of the combined modes of deformation of the blade as a complex structural part and their effects on the aerodynamic loads, it constitutes a substantial advancement ahead the state-of-the-art aeroelastic models currently available, like the FAST-Aerodyn suite. In this thesis, we also include the results of several experiments on the NREL-5MW blade, which is widely accepted today as a benchmark blade, together with some modifications intended to explore the capacities of the new code in terms of capturing features on blade-dynamic behavior, which are normally overlooked by the existing aeroelastic models.