326 research outputs found

    Responding to \u3ci\u3eHerrera v. Collins\u3c/i\u3e: Ensuring That Innocents are Not Executed

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    Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme

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    A compressible flow code that can predict the nonlinear unsteady aerodynamics associated with transonic flows over oscillating cascades is developed and validated. The code solves the two dimensional, unsteady Euler equations using a time-marching, flux-difference splitting scheme. The unsteady pressures and forces can be determined for arbitrary input motions, although only harmonic pitching and plunging motions are addressed. The code solves the flow equations on a H-grid which is allowed to deform with the airfoil motion. Predictions are presented for both flat plate cascades and loaded airfoil cascades. Results are compared to flat plate theory and experimental data. Predictions are also presented for several oscillating cascades with strong normal shocks where the pitching amplitudes, cascade geometry and interblade phase angles are varied to investigate nonlinear behavior

    A communications model for an ISAS to NASA span link

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    The authors propose that an initial computer-to-computer communication link use the public packet switched networks (PPSN) Venus-P in Japan and TELENET in the U.S. When the traffic warrants it, this link would then be upgraded to a dedicated leased line that directly connects into the Space Physics Analysis Network (SPAN). The proposed system of hardware and software will easily support migration to such a dedicated link. It therefore provides a cost effective approach to the network problem. Once a dedicated line becomes operation it is suggested that the public networks link and continue to coexist, providing a backup capability

    Social Capital Impact On Service Supply Chains

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    Purpose This study explores the impact of social capital on service firm supply chains.Design/methodology/approach The theoretical underpinnings of social capital is reviewed from various disciplines, including sociology, management, and operations management. This is used to develop a conceptual model of the use of social capital in a service supply chain setting.Findings - Social capital is proposed to improve the operational performance of service firms as a source of both physical and information resources. The impact of social capital is projected to vary by firm size and service type. Small firms have limited resources and thus a need for resources obtained through social capital. Service firms that have high customization and customer contact are subject to process variations which can be mitigated by social capital. A conceptual model is presented to test several propositions related to social capital.Originality/value The impact of social capital has not been widely studied in an operational setting. This is the first known study to specifically analyze the impact of social capital in service supply chains

    SPAN: Astronomy and astrophysics

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    The Space Physics Analysis Network (SPAN) is a multi-mission, correlative data comparison network which links science research and data analysis computers in the U.S., Canada, and Europe. The purpose of this document is to provide Astronomy and Astrophysics scientists, currently reachable on SPAN, with basic information and contacts for access to correlative data bases, star catalogs, and other astrophysic facilities accessible over SPAN

    Flutter analysis of supersonic axial flow cascades using a high resolution Euler solver. Part 1: Formulation and validation

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    This report presents, in two parts, a dynamic aeroelastic stability (flutter) analysis of a cascade of blades in supersonic axial flow. Each blade of the cascade is modeled as a typical section having pitching and plunging degrees of freedom. Aerodynamic forces are obtained from a time accurate, unsteady, two-dimensional cascade solver based on the Euler equations. The solver uses a time marching flux-difference splitting (FDS) scheme. Flutter stability is analyzed in the frequency domain. The unsteady force coefficients required in the analysis are obtained by harmonically oscillating (HO) the blades for a given flow condition, oscillation frequency, and interblade phase angle. The calculated time history of the forces is then Fourier decomposed to give the required unsteady force coefficients. An influence coefficient (IC) method and a pulse response (PR) method are also implemented to reduce the computational time for the calculation of the unsteady force coefficients for any phase angle and oscillation frequency. Part 1, this report, presents these analysis methods and their validation by comparison with results obtained from linear theory for a selected flat plate cascade geometry. A typical calculation for a rotor airfoil is also included to show the applicability of the present solver for airfoil configurations. The predicted unsteady aerodynamic forces for a selected flat plate cascade geometry and flow conditions correlated well with those obtained from linear theory for different interblade phase angles and oscillation frequencies. All the three methods of predicting unsteady force coefficients, namely, HO, IC, and PR, showed good correlations with each other. It was established that only a single calculation with four blade passages is required to calculate the aerodynamic forces for any phase angle for a cascade consisting of any number of blades, for any value of the oscillation frequency. Flutter results, including mistuning effects, for a cascade of stator airfoils are presented in Part 2 of the report

    Deflection Effects in Inner-Shell Ionization

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    Journals published by the American Physical Society can be found at http://publish.aps.org

    Inner-Shell Charge-Transfer in Asymmetric Ion-Atom Collisions

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    Journals published by the American Physical Society can be found at http://publish.aps.org
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