1,056,202 research outputs found

    WTS-4 system verification unit for wind/hydroelectric integration study

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    The Bureau of Reclamation (Reclamation) initiated a study to investigate the concept of integrating 100 MW of wind energy from megawatt-size wind turbines with the Federal hydroelectric system. As a part of the study, one large wind turbine was purchased through the competitive bid process and is now being installed to serve as a system verification unit (SVU). Reclamation negotiated an agreement with NASA to provide technical management of the project for the design, fabrication, installation, testing, and initial operation. Hamilton Standard was awarded a contract to furnish and install its WTS-4 wind turbine rated at 4 MW at a site near Medicine Bow, Wyoming. The purposes for installing the SVU are to fully evaluate the wind/hydro integration concept, make technical evaluation of the hardware design, train personnel in the technology, evaluate operation and maintenance aspects, and evaluate associated environmental impacts. The SVU will be operational in June 1982. Data from the WTS-4 and from a second SVU, Boeing's MOD-2, will be used to prepare a final design for a 100-MW farm if Congress authorizes the project

    Army-NASA aircrew/aircraft integration program. Phase 5: A3I Man-Machine Integration Design and Analysis System (MIDAS) software concept document

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    This is the Software Concept Document for the Man-machine Integration Design and Analysis System (MIDAS) being developed as part of Phase V of the Army-NASA Aircrew/Aircraft Integration (A3I) Progam. The approach taken in this program since its inception in 1984 is that of incremental development with clearly defined phases. Phase 1 began in 1984 and subsequent phases have progressed at approximately 10-16 month intervals. Each phase of development consists of planning, setting requirements, preliminary design, detailed design, implementation, testing, demonstration and documentation. Phase 5 began with an off-site planning meeting in November, 1990. It is expected that Phase 5 development will be complete and ready for demonstration to invited visitors from industry, government and academia in May, 1992. This document, produced during the preliminary design period of Phase 5, is intended to record the top level design concept for MIDAS as it is currently conceived. This document has two main objectives: (1) to inform interested readers of the goals of the MIDAS Phase 5 development period, and (2) to serve as the initial version of the MIDAS design document which will be continuously updated as the design evolves. Since this document is written fairly early in the design period, many design issues still remain unresolved. Some of the unresolved issues are mentioned later in this document in the sections on specific components. Readers are cautioned that this is not a final design document and that, as the design of MIDAS matures, some of the design ideas recorded in this document will change. The final design will be documented in a detailed design document published after the demonstrations

    Aeroservoelastic Testing of Free Flying Wind Tunnel Models Part 1: A Sidewall Supported Semispan Model Tested for Gust Load Alleviation and Flutter Suppression

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    of a two part document. Part 2 is titled: "Aeroservoelastic Testing of Free Flying Wind Tunnel Models, Part 2: A Centerline Supported Fullspan Model Tested for Gust Load Alleviation." A team comprised of the Air Force Research Laboratory (AFRL), Northrop Grumman, Lockheed Martin, and the NASA Langley Research Center conducted three aeroservoelastic wind tunnel tests in the Transonic Dynamics Tunnel to demonstrate active control technologies relevant to large, flexible vehicles. In the first of these three tests, a semispan, aeroelastically scaled, wind tunnel model of a flying wing SensorCraft vehicle was mounted to a force balance to demonstrate gust load alleviation. In the second and third tests, the same wing was mated to a new, multi-degree of freedom, sidewall mount. This mount allowed the half-span model to translate vertically and pitch at the wing root, allowing better simulation of the full span vehicle's rigid body modes. Gust load alleviation (GLA) and Body freedom flutter (BFF) suppression were successfully demonstrated. The rigid body degrees-of-freedom required that the model be flown in the wind tunnel using an active control system. This risky mode of testing necessitated that a model arrestment system be integrated into the new mount. The safe and successful completion of these free flying tests required the development and integration of custom hardware and software. This paper describes the many systems, software, and procedures that were developed as part of this effort

    An Open Virtual World for Professional Development

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    The paper presents a study that focuses on the issue of sup-porting educational experts to choose the right combination of educational methodology and technology tools when designing training and learning programs. It is based on research in the field of adaptive intelligent e-learning systems. The object of study is the professional growth of teachers in technology and in particular that part of their qualification which is achieved by organizing targeted training of teachers. The article presents the process of creating and testing a system to support the decision on the design of training for teachers, leading to more effective implementation of technology in education and integration in diverse educational contexts. ACM Computing Classification System (1998): H.4.2, I.2.1, I.2, I.2.4, F.4.1.∗This article presents the principal results of the Ph.D. thesis Open Virtual Worlds for Professional Development by Eliza Stefanova (Faculty of Mathematics and Informatics at Sofia University), successfully defended at the Specialized Academic Council of FMI on 10 December, 2012

    Is This Going to Be the End? Understanding Problematic Integration Among Appalachian Patients in Colorectal Cancer Screening Navigation

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    Colorectal cancer (CRC) is preventable through regular screening; however, incidence and mortality rates in Appalachia are among the highest in the United States. Public health programs and interventions meant to mitigate the higher CRC burden and increase screening rates are ongoing in the U.S. and Appalachia. In continuing the efforts to reduce the burden of CRC in Appalachian communities, this dissertation uses a two-part study to investigate communication practices relative to problematic integration and health beliefs in CRC screening conversations from the perspective of both patients and patient navigators in the region. As part of efforts directed by the Rural Cancer Prevention Center (RCPC; 2009-2019), patients who received a positive fecal immunochemical test (FIT) and the patient navigators assigned to connect them with direct visualization follow-up testing were interviewed one-on-one to better understand the role of problematic integration in CRC screening communication. Study 1 investigates patient navigators\u27 (n = 9) perspectives of their efforts to connect patients with appropriate CRC screening, while Study 2 analyzes the accounts of patients (n = 10) with positive FIT who refused follow- up colonoscopy testing (at the time of recruitment) after engaging in patient navigation services. With problematic integration theory and the health belief model as a guide, data from these two studies in the Appalachian Kentucky context support an overarching model for how patient navigators and patients address uncertainty in CRC screening. Analyzing these phenomena at the intersection of communication and health behavior theories highlights the utility of health communication research expertise in guiding interventions across the healthcare continuum. In addition, data from the studies may be used to understand the nature of participation in CRC screening conversations and how these dynamics contribute to patient-centered care and shared decision-making, which is especially important with the additional challenges for screening exacerbated by a global COVID-19 pandemic. The findings from these studies are discussed in terms of contributing to more effective clinical and patient navigation communication practices and providing public health practitioners with essential considerations for shaping interventions to support shared decision-making and improve CRC screening rates in similar populations

    NEXT Propellant Management System Integration With Multiple Ion Thrusters

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    As a critical part of the NEXT test validation process, a multiple-string integration test was performed on the NEXT propellant management system and ion thrusters. The objectives of this test were to verify that the PMS is capable of providing stable flow control to multiple thrusters operating over the NEXT system throttling range and to demonstrate to potential users that the NEXT PMS is ready for transition to flight. A test plan was developed for the sub-system integration test for verification of PMS and thruster system performance and functionality requirements. Propellant management system calibrations were checked during the single and multi-thruster testing. The low pressure assembly total flow rates to the thruster(s) were within 1.4 percent of the calibrated support equipment flow rates. The inlet pressures to the main, cathode, and neutralizer ports of Thruster PM1R were measured as the PMS operated in 1-thruster, 2-thruster, and 3-thruster configurations. It was found that the inlet pressures to Thruster PM1R for 2-thruster and 3-thruster operation as well as single thruster operation with the PMS compare very favorably indicating that flow rates to Thruster PM1R were similar in all cases. Characterizations of discharge losses, accelerator grid current, and neutralizer performance were performed as more operating thrusters were added to the PMS. There were no variations in these parameters as thrusters were throttled and single and multiple thruster operations were conducted. The propellant management system power consumption was at a fixed voltage to the DCIU and a fixed thermal throttle temperature of 75 C. The total power consumed by the PMS was 10.0, 17.9, and 25.2 W, respectively, for single, 2-thruster, and 3-thruster operation with the PMS. These sub-system integration tests of the PMS, the DCIU Simulator, and multiple thrusters addressed, in part, the NEXT PMS and propulsion system performance and functionality requirements

    Efficient dynamic resampling for dominance-based multiobjective evolutionary optimization

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    Multi-objective optimization problems are often subject to the presence of objectives that require expensive resampling for their computation. This is the case for many robustness metrics, which are frequently used as an additional objective that accounts for the reliability of specific sections of the solution space. Typical robustness measurements use resampling, but the number of samples that constitute a precise dispersion measure has a potentially large impact on the computational cost of an algorithm. This article proposes the integration of dominance based statistical testing methods as part of the selection mechanism of evolutionary multi-objective genetic algorithms with the aim of reducing the number of fitness evaluations. The performance of the approach is tested on five classical benchmark functions integrating it into two well-known algorithms, NSGA-II and SPEA2. The experimental results show a significant reduction in the number of fitness evaluations while, at the same time, maintaining the quality of the solutions.The authors acknowledge financial support granted by the Spanish Ministry of Economy and Competitivity under grant ENE2014-56126-C2-2-R

    Contact effects in thermally evaporated pentacene thin films and aspects of microsystem hybrid integration

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    Organic thin film transistors have the potential to replace silicon based transistors in applications such as smart cards and RF-ID due to their low cost and low processing temperatures. Thermally evaporated pentacene is studied as an organic thin film material. Thin film transistors were fabricated in bottom contact structure using thermal evaporation of pentacene at a rate of 0.5 to 1 nm/s. Heavily doped Si was used as a gate material and 100 nm thick silicon dioxide was used as a dielectric. Ni was used as contact metal for source and drain contacts. Threshold voltage of 16 V and mobility of 0.0016 cm2/V-s were obtained. Grain size in pentacene films increased from 120 nm to 150 nm upon annealing at 200 ◦C for 30 min. in nitrogen ambient. Resistivity of the pentacene films decreased with annealing temperature indicating an activation energy of 0.22 eV. Hybrid Integration of a Bio-implantable Electrical Stimulation System (BESS) is carried out in the second part of this work. BESS produces periodic pulses that stimulate the gastric muscles. BESS consists of an application specific integrated circuit powered by rechargeable batteries, which are charged by a remote power delivery system. Screen printing technique was used for BESS hybrid integration. The same can be extended in future for fabricating organic transistors. The optimum screen printing process determined included squeegee speed of 2.2 cm/s, off-contact height of 2 mm and squeegee pressure of 80 PSI for ED3000 ink used. Ceramic, silicon, glass, polyimide and kapton substrates have been utilized for printing. Interconnect pattern of area 1” × 0.75” was screen printed on a ceramic substrate using ED3000 silver conductive ink and surface mount components were mounted. Bio-compatible 100 µm thick polyimide substrates were prepared by spin coating pyralin at 750 RPM and baked at 350 ◦C for 30 min. ED3000 conductive ink was used to print electrodes on polyimide substrates. The BESS system is now ready for full hybrid integration and testing

    Minibix: Item banking with web services

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    The Minibix system was developed from an existing prototype item bank system in use for high-stakes testing at the University of Cambridge. The system has been developed over the last year with support from the JISC e- Learning Programme. This project has redeveloped the system based on version 2 of the IMS Question and Test Interoperability (QTI) specification and is publishing the resulting system under an open source license. In this paper, we propose a simple service model for describing the authoring, banking, test construction and delivery of assessment content. The item banking model is implemented by the Minibix system and will be demonstrated in conjunction with authoring, test construction and delivery systems developed by the sister projects: AQuRate (Kingston University) and AsDel (University of Southampton). These services, as part of a wider e-Framework, could enable tool integration on a scale suitable for interacting with large-scale item banks. Private banks are already used routinely in high-stakes summative assessment but open repositories of items for formative use are now becoming available. For example, the E3AN item bank for Electrical and Electronic Engineering or the item bank for the Physical Sciences recently announced by the HEA

    Field testing, validation and optimization report

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    The COMMON SENSE project has been designed and planned in order to meet the general and specific scientific and technical objectives mentioned in its Description of Work (page 77). As the overall strategy, the 11 work packages (WPs) of the work plan were grouped into 3 key phases: (1) RD basis for cost-effective sensor development , (2) Sensor development, sensor web platform and integration, and (3) Field testing. In the first two phases, partners involved in WP1 and WP2 have provided a general understanding and integrated basis for a cost effective sensors development. Within the following WPs 4 to 8 the new sensors were created and integrated into different identified platforms. During the third phase of field testing (WP9), partners have deployed precompetitive prototypes at chosen platforms (e.g. research vessels, oil platforms, buoys and submerged moorings, ocean racing yachts, drifting buoys). Starting from August 2015 (month 22; task 9.2), these platforms have allowed the partnership to test the adaptability and performance of the in-situ sensors and verify if the transmission of data is properly made, correcting deviations. In task 9.1 all stakeholders identified in WP2 have been contacted in order to agree upon a coordinated agenda for the field testing phase for each of the platforms. Field testing procedures (WP2) and deployment specificities, defined during sensor development in WPs 4 to 8, have been closely studied by all stakeholders involved in field testing activities in order for everyone to know their role, how to proceed and to provide themselves with the necessary material and equipment (e.g. transport of instruments). All this information have provided the basis for designing and coordinating field testing activities. Subsequently, the available new sensors have been tested since August 2015 till mid-October of the current year (2016) as part of task 9.2, following the indications defined in D9.1, such as the intercomparison of the new sensors with commercial ones, when possible. The availability of new sensors was quite different in time starting with the first tests in September and October 2015 on noise, nutrient and heavy metals sensors and closing with pCO2 in late September 2016. Sensors are technically fully described in the deliverables of WPs 3 to 8 and are here just mentioned where necessary. For further details, please consider those reports. Objectives and rationale The protocols prepared in D9.1 have been verified during the field testing activities of the innovative sensors on platforms. These can be summarized into 3 categories: (1) Research vessels (regular cruises); (2) Fixed platforms; (3) Ocean racing yachts. An exhaustive analysis of the different data obtained during field testing activities has been carried on in order to set possible optimization actions for prototypes design and performances. The data from each platform have been analyzed to verify limits and optimal installations or possible improvements. Finally a set of possible optimization actions has been defined. Data and observations collected during the course of field testing have been used to iteratively optimize the design and performance of the precompetitive prototypes
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