2,434 research outputs found

    Implementation of a Virtual Journal Club in a Clinical Nursing Setting

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    Healthcare practice is increasingly focused on delivering care that is based on published research evidence. Staff development nurses can institute journal clubs to teach nursing staff critical appraisal of research articles and ways to translate research findings into clinical practice. Unfortunately, attending meetings regularly is often a challenge for nurses, and relatively few have the knowledge and expertise to adequately critique research articles. One way to bridge the limitations of accessibility and limited research expertise of journal club members is to establish a virtual journal club. This article describes one hospital\u27s experience with developing a virtual journal club

    Mesh ratios for best-packing and limits of minimal energy configurations

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    For NN-point best-packing configurations ωN\omega_N on a compact metric space (A,ρ)(A,\rho), we obtain estimates for the mesh-separation ratio γ(ωN,A)\gamma(\omega_N,A), which is the quotient of the covering radius of ωN\omega_N relative to AA and the minimum pairwise distance between points in ωN\omega_N. For best-packing configurations ωN\omega_N that arise as limits of minimal Riesz ss-energy configurations as ss\to \infty, we prove that γ(ωN,A)1\gamma(\omega_N,A)\le 1 and this bound can be attained even for the sphere. In the particular case when N=5 on S2S^2 with ρ\rho the Euclidean metric, we prove our main result that among the infinitely many 5-point best-packing configurations there is a unique configuration, namely a square-base pyramid ω5\omega_5^*, that is the limit (as ss\to \infty) of 5-point ss-energy minimizing configurations. Moreover, γ(ω5,S2)=1\gamma(\omega_5^*,S^2)=1

    An inventory of aeronautical ground research facilities. Volume 1: Wind tunnels

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    A survey of wind tunnel research facilities in the United States is presented. The inventory includes all subsonic, transonic, and hypersonic wind tunnels operated by governmental and private organizations. Each wind tunnel is described with respect to size, mechanical operation, construction, testing capabilities, and operating costs. Facility performance data are presented in charts and tables

    An inventory of aeronautical ground research facilities. Volume 3: Structural

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    An inventory of test facilities for conducting acceleration, environmental, impact, structural shock, load, heat, vibration, and noise tests is presented. The facility is identified with a description of the equipment, the testing capabilities, and cost of operation. Performance data for the facility are presented in charts and tables
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