1,076 research outputs found

    An Analytical Study for Subsonic Oblique Wing Transport Concept

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    The oblique wing concept has been investigated for subsonic transport application for a cruise Mach number of 0.95. Three different mission applications were considered and the concept analyzed against the selected mission requirements. Configuration studies determined the best area of applicability to be a commercial passenger transport mission. The critical parameter for the oblique wing concept was found to be aspect ratio which was limited to a value of 6.0 due to aeroelastic divergence. Comparison of the concept final configuration was made with fixed winged configurations designed to cruise at Mach 0.85 and 0.95. The crossover Mach number for the oblique wing concept was found to be Mach 0.91 for takeoff gross weight and direct operating cost. Benefits include reduced takeoff distance, installed thrust and mission block fuel and improved community noise characteristics. The variable geometry feature enables the final configuration to increase range by 10% at Mach 0.712 and to increase endurance by as much as 44%

    United We Stand: A Case Study about Increasing Equity in the Capacity Building Grant Funding Process for United Way of Greater Richmond and Petersburg

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    In response to a problem of practice presented by the United Way of Greater Richmond and Petersburg, this case study addresses equity in the grant funding and capacity development processes and how small, emergent, grassroots, minority-led nonprofit organizations in one Virginia region are affected. Through the lens of Systems Informed Positive Psychology (SIPP), a convergent mixed-methods approach was used to holistically explore the challenges and needs that these particular nonprofits face. Data was obtained through community conversations which included focus groups, individual interviews, and an online questionnaire coupled with Shumate et al.’s (2017) Nonprofit Capacities Instrument, a validated 45-item survey that provides a benchmark in eight different interrelated dimensions of organizational capacity based on the self-report of participants. We found that these organizations are collectively encountering widespread structural and systemic racism, bureaucratic complexity, and a lack of access to resources as well as relational gaps between themselves and funding agencies. As a result of these challenges, they require change in the historical system, practices, and processes of local philanthropic entities along with open and transparent communication between funders and grantees in conjunction with the cultivation of trust-based relationships which support community resiliency through a humanist commitment. Such findings demonstrate the need for the co-creation of an egalitarian and equitable grant funding model between grantor and grantees utilizing the tenets of a more equitably evolved Collective Impact Framework. Findings from our study also raise empirical, practical, and theoretical implications that warrant future consideration particularly regarding the lack of attention and cultural understanding given to minority-led nonprofit organizations and the trauma-informed care which is needed to support them in serving their communities. Findings also indicate that there is a significant opportunity for the philanthropic sector to mirror recent advancements in education and become more community-and human-centered in the structures, processes, and decisions that are made, which requires systemic change

    Search for axion-like particles using a variable baseline photon regeneration technique

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    We report the first results of the GammeV experiment, a search for milli-eV mass particles with axion-like couplings to two photons. The search is performed using a "light shining through a wall" technique where incident photons oscillate into new weakly interacting particles that are able to pass through the wall and subsequently regenerate back into detectable photons. The oscillation baseline of the apparatus is variable, thus allowing probes of different values of particle mass. We find no excess of events above background and are able to constrain the two-photon couplings of possible new scalar (pseudoscalar) particles to be less than 3.1x10^{-7} GeV^{-1} (3.5x10^{-7} GeV^{-1}) in the limit of massless particles.Comment: 5 pages, 4 figures. This is the version accepted by PRL and includes updated limit

    A Map-Reduce Parallel Approach to Automatic Synthesis of Control Software

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    Many Control Systems are indeed Software Based Control Systems, i.e. control systems whose controller consists of control software running on a microcontroller device. This motivates investigation on Formal Model Based Design approaches for automatic synthesis of control software. Available algorithms and tools (e.g., QKS) may require weeks or even months of computation to synthesize control software for large-size systems. This motivates search for parallel algorithms for control software synthesis. In this paper, we present a Map-Reduce style parallel algorithm for control software synthesis when the controlled system (plant) is modeled as discrete time linear hybrid system. Furthermore we present an MPI-based implementation PQKS of our algorithm. To the best of our knowledge, this is the first parallel approach for control software synthesis. We experimentally show effectiveness of PQKS on two classical control synthesis problems: the inverted pendulum and the multi-input buck DC/DC converter. Experiments show that PQKS efficiency is above 65%. As an example, PQKS requires about 16 hours to complete the synthesis of control software for the pendulum on a cluster with 60 processors, instead of the 25 days needed by the sequential algorithm in QKS.Comment: To be submitted to TACAS 2013. arXiv admin note: substantial text overlap with arXiv:1207.4474, arXiv:1207.409

    C-5A/orbiter wind tunnel testing and analysis: Piggyback ferry

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    Wind tunnel testing and analytical studies of the feasibility of ferrying the NASA Shuttle Orbiter on the C-5A in a piggyback mode have been accomplished. Testing was conducted in the 8x12 foot low speed wind tunnel using an existing 0.0399 scale C-5A model in conjunction with a NASA 0.0405 scale Orbiter model. Six component force and moment data were measured over a range of pitch and yaw angles to determine lift and drag characteristics, lateral/directional stability characteristics and longitudinal and directional control powers. A description of the wind tunnel test program with a run schedule and the complete plotted data for all the test runs are presented. Initial emphasis was given to determining the effects of the Orbiter above the C-5A and the optimum location for minimum interference on C-5A characteristics. A comprehensive series of cruise configurations were tested including a range of Orbiter longitudinal and vertical locations, incidences, and afterbody fairings. Subsequently, a series of configurations were devised during the test program to determine means of recovering directional stability degradation due to Orbiter interference
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