1,779 research outputs found

    Policing Celebratory Behavior: Tactical vs. Relationship, a Micro Study of Lexington Kentucky Police Response

    Get PDF
    In the last three plus decades, considerable attention has been given to certain common phases in the life cycle of gatherings, demonstrations, and riots in the United States. Much of the study focuses on theoretical origin and social psychology associated with each type of event. There is considerably less empirical work regarding police reaction to these events, particularly concerning celebratory behavior following a sporting event. Celebratory incidents are less organized than their protests counterpart. A variety of fans with collective zeal gather in a common location without leadership or mission. Celebratory behavior has become commonplace amongst fans in cities with sports teams competing for prestigious victories in nearly all types of sporting contests. Post-game celebration may have a ritualized aspect and be institutionalized, in the sense that participants and controllers expect them to happen. For public order maintenance, the strategic orientation used by police for celebratory crowds following these events has predominantly been paramilitary in nature both from an appearance and behavior aspect. Some research and social theory argue that a systemic culture of militarization in American police makes these incidents worse. To aid in this research a micro level case study from Lexington, Kentucky will examine post-games from two Final Four tournament years of celebratory behavior and the evolving strategies of police. Brief comparisons of police response from other agencies are discussed and analyzed with Lexington police response. Evolving police tactics and social theory combine to suggest that a relationship oriented response may be favored over a tactical approach to reduce crowd agitation or aggressive behavior during post-game celebration. Finally, considerations of police tactics toward a more relationship-oriented response are discussed

    Exploring the Motivational Factors that Empower Military Spouses to Pursue Degrees in Higher Education

    Get PDF
    This study aimed to explore the factors that motivate and empower military spouses to persist in pursuing degrees in higher education. The following research question guided this study? What do military spouses perceive as the factors that motivate and empower them to persist in earning college degrees? Fifteen military spouses participated in this study. The military spouses who participated in the study shared their experiences on motivating factors that empowered them to continue earning a college degree. The theory of Cultural Capital was used as the theoretical framework to guide the concept that the military environment is a culture within a culture and that they bring this knowledge and experience into the classroom

    Performance and Stability Analyses of Rocket Thrust Chambers with Oxygen/Methane Propellants

    Get PDF
    Liquid rocket engines using oxygen and methane propellants are being considered by the National Aeronautics and Space Administration (NASA) for future in-space vehicles. This propellant combination has not been previously used in flight-qualified engine systems developed by NASA, so limited test data and analysis results are available at this stage of early development. As part of activities for the Propulsion and Cryogenic Advanced Development (PCAD) project funded under the Exploration Technology Development Program, the NASA Marshall Space Flight Center (MSFC) has been evaluating capability to model combustion performance and stability for oxygen and methane propellants. This activity has been proceeding for about two years and this paper is a summary of results to date. Hot-fire test results of oxygen/methane propellant rocket engine combustion devices for the modeling investigations have come from several sources, including multi-element injector tests with gaseous methane from the 1980s, single element tests with gaseous methane funded through the Constellation University Institutes Program, and multi-element injector tests with both gaseous and liquid methane conducted at the NASA MSFC funded by PCAD. For the latter, test results of both impinging and coaxial element injectors using liquid oxygen and liquid methane propellants are included. Configurations were modeled with two one-dimensional liquid rocket combustion analysis codes, the Rocket Combustor Interactive Design and Analysis code and the Coaxial Injector Combustion Model. Special effort was focused on how these codes can be used to model combustion and performance with oxygen/methane propellants a priori, and what anchoring or calibrating features need to be applied, improved or developed in the future. Low frequency combustion instability (chug) occurred, with frequencies ranging from 150 to 250 Hz, with several multi-element injectors with liquid/liquid propellants, and was modeled using techniques from Wenzel and Szuch. High-frequency combustion instability also occurred at the first tangential (1T) mode, at about 4500 Hz, with several multi-element injectors with liquid/liquid propellants. Analyses of the transverse mode instability were conducted by evaluating injector resonances and empirical methods developed by Hewitt

    SKITTER foot design

    Get PDF
    A mechanical design team was formed to design a foot for the lunar utility vehicle SKITTER. The primary design was constrained to be a ski pole design compatible with the existing femur-tibia design legs. The lunar environment had several important effects on the foot design. Three materials were investigated for the SKITTER foot: aluminum alloys, cold worked stainless steel alloys, and titanium alloys. Thin film coatings were investigated as a method of wear reduction for the foot. The performance of the foot is dependent on the action of the legs. The range of motion for the legs was determined to be vertical to 15 degrees above horizontal. An impact analysis was performed for the foot movement, but the results were determined to be inconclusive due to unknown soil parameters. The initial foot design configuration consisted of an annulus attached to the pointed pole. The annulus was designed to prevent excess sinkage. Later designs call for a conical shaped foot with a disk at the point of the tibia attachment. The conical design was analyzed for strength and deflection by two different approaches. A deformable body analysis was performed for the foot under crane load in crane position, and also under actuator load in the vertical position. In both cases, the deflection of the foot was insignificant and the stresses well below the strength of the titanium alloy

    Ultra-compact dwarf galaxies: a new class of compact stellar system discovered in the Fornax Cluster

    Get PDF
    We have used the 2dF spectrograph on the Anglo-Australian Telescope to obtain a complete spectroscopic sample of all objects in the magnitude range, Bj= 16.5 to 19.8, regardless of morphology, in an area centred on the Fornax Cluster of galaxies. Among the unresolved targets are five objects which are members of the Fornax Cluster. They are extremely compact stellar systems with scale lengths less than 40 parsecs. These ultra-compact dwarfs are unlike any known type of stellar system, being more compact and significantly less luminous than other compact dwarf galaxies, yet much brighter than any globular cluster.Comment: To appear in IAU Symposium 207: Extragalactic Star Cluster

    Local Heat Flux Measurements with Single and Small Multi-element Coaxial Element-Injectors

    Get PDF
    To support NASA's Vision for Space Exploration mission, the NASA Marshall Space Flight Center conducted a program in 2005 to improve the capability to predict local thermal compatibility and heat transfer in liquid propellant rocket engine combustion devices. The ultimate objective was to predict and hence reduce the local peak heat flux due to injector design, resulting in a significant improvement in overall engine reliability and durability. Such analyses are applicable to combustion devices in booster, upper stage, and in-space engines with regeneratively cooled chamber walls, as well as in small thrust chambers with few elements in the injector. In this program, single and three-element injectors were hot-fire tested with liquid oxygen and gaseous hydrogen propellants at The Pennsylvania State University Cryogenic Combustor Laboratory from May to August 2005. Local heat fluxes were measured in a 1-inch internal diameter heat sink combustion chamber using Medtherm coaxial thermocouples and Gardon heat flux gauges, Injector configurations were tested with both shear coaxial elements and swirl coaxial elements. Both a straight and a scarfed single element swirl injector were tested. This paper includes general descriptions of the experimental hardware, instrumentation, and results of the hot-fire testing for three coaxial shear and swirl elements. Detailed geometry and test results the for shear coax elements has already been published. Detailed test result for the remaining 6 swirl coax element for the will be published in a future JANNAF presentation to provide well-defined data sets for development and model validation

    Found: High Surface Brightness Compact Galaxies

    Full text link
    We are using the 2dF spectrograph to make a survey of all objects (`stars' and `galaxies') in a 12 sq.deg region towards the Fornax cluster. We have discovered a population of compact emission-line galaxies unresolved on photographic sky survey plates and therefore missing in most galaxy surveys based on such material. These galaxies are as luminous as normal field galaxies. Using H-alpha to estimate star formation they contribute at least an additional 5 per cent to the local star formation rate.Comment: To appear in "The Low Surface Brightness Universe", IAU Coll 171, eds. J.I. Davies et al., A.S.P. Conference Series. 3 pages, LaTex, 1 encapsulated ps-figure, requires paspconf.st
    corecore