2,880 research outputs found

    RSM 1.0 user's guide: A resupply scheduler using integer optimization

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    The Resupply Scheduling Model (RSM) is a PC based, fully menu-driven computer program. It uses integer programming techniques to determine an optimum schedule to replace components on or before a fixed replacement period, subject to user defined constraints such as transportation mass and volume limits or available repair crew time. Principal input for RSJ includes properties such as mass and volume and an assembly sequence. Resource constraints are entered for each period corresponding to the component properties. Though written to analyze the electrical power system on the Space Station Freedom, RSM is quite general and can be used to model the resupply of almost any system subject to user defined resource constraints. Presented here is a step by step procedure for preparing the input, performing the analysis, and interpreting the results. Instructions for installing the program and information on the algorithms are given

    Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Deg

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    A flight investigation was made at altitudes of 40,000, 25,000 and 15,000 feet to determine the horizontal-tail loads of the Bell X-5 research airplane at a sweep angle of 58.7 deg over the lift range of the airplane for Mach numbers from 0.61 to 1.00. The horizontal-tail loads were found to be nonlinear with lift throughout the lift ranges tested at all Mach numbers except at a Mach number of 1.00. The balancing tail loads reflected the changes which occur in the wing characteristics with increasing angle of attack. The nonlinearities were, in general, more pronounced at the higher angles of attack near the pitch-up where the balancing tail loads indicate that the wing-fuselage combination becomes unstable. No apparent effects of altitude on the balancing tail loads were evident over the comparable lift ranges of these tests at altitudes from 40,000 feet to 15,000 feet. Comparisons of balancing tail loads obtained from flight and windtunnel tests indicated discrepancies in absolute magnitudes, but the general trends of the data agree. Some differences in absolute magnitude may be accounted for by the tail load carried inboard of the strain-gage station and the load induced on the fuselage by the presence of the tail. These loads were not measured in flight

    Spectral shift function for operators with crossed magnetic and electric fields

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    We obtain a representation formula for the derivative of the spectral shift function ξ(λ;B,ϵ)\xi(\lambda; B, \epsilon) related to the operators H0(B,ϵ)=(DxBy)2+Dy2+ϵxH_0(B,\epsilon) = (D_x - By)^2 + D_y^2 + \epsilon x and H(B,ϵ)=H0(B,ϵ)+V(x,y),B>0,ϵ>0H(B, \epsilon) = H_0(B, \epsilon) + V(x,y), \: B > 0, \epsilon > 0. We establish a limiting absorption principle for H(B,ϵ)H(B, \epsilon) and an estimate O(ϵn2){\mathcal O}(\epsilon^{n-2}) for ξ(λ;B,ϵ)\xi'(\lambda; B, \epsilon), provided λσ(Q)\lambda \notin \sigma(Q), where $Q = (D_x - By)^2 + D_y^2 + V(x,y).

    Portable Computers Used in Respiratory Care Charting

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    journal articleBiomedical Informatic

    Bibliography of Graduate Theses: Fort Hays Kansas State College 1930-1970

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    It is the hope that this publication will serve to inform the academic community, and the prospective graduate student in particular, of the range of research interest and opportunities in the graduate division at Fort Hays Kansas State College. The index is alphabetically arranged by author with a numerical reference to the thesis as listed under subject fields.https://scholars.fhsu.edu/fort_hays_studies_series/1030/thumbnail.jp

    Computer Charting: An Evaluation of a Respiratory Care Computer System

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    journal articleBiomedical Informatic

    Military Use of the Space Shuttle

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    There is little doubt that the Space Shuttle will provide a quantum jump in man\u27s activity in space. It will provide the means to make the transition from primarily machine-oriented space activities to man-orientated activities. Man\u27s activities will move from exploratory to exploitative. The purpose of this article is to examine the military aspects of this transition in the context of the legal regime of outer space that has evolved in the more than two decades since the orbiting of Sputnik I. Is the prospect of increased military activities and capabilities compatible with this regime or conversely, does the legal regime restrict military activities in space and if so, what are those restrictions? A discussion of this type must of necessity include, in addition to the legal principles involved, a discussion of our national space policy and our present and future military use of space. Moreover, since international law evolves from the practice of States and is attuned to the realities of world politics and power, any discussion of the military use of space would be incomplete without a discussion of the military space programs of the Soviet Union and its view regarding the legality of the military use of space

    Limiting absorption principle for the dissipative Helmholtz equation

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    Adapting Mourre's commutator method to the dissipative setting, we prove a limiting absorption principle for a class of abstract dissipative operators. A consequence is the resolvent estimates for the high frequency Helmholtz equation when trapped trajectories meet the set where the imaginary part of the potential is non-zero. We also give the resolvent estimates in Besov spaces
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