30,323 research outputs found

    The atmospheric effects of stratospheric aircraft

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    This document presents a second report from the Atmospheric Effects of Stratospheric Aircraft (AESA) component of NASA's High-Speed Research Program (HSRP). This document presents a second report from the Atmospheric Effects of Stratospheric Aircraft (AESA) component of NASA's High Speed Research Program (HSRP). Market and technology considerations continue to provide an impetus for high-speed civil transport research. A recent United Nations Environment Program scientific assessment has shown that considerable uncertainty still exists about the possible impact of aircraft on the atmosphere. The AESA was designed to develop the body of scientific knowledge necessary for the evaluation of the impact of stratospheric aircraft on the atmosphere. The first Program report presented the basic objectives and plans for AESA. This second report presents the status of the ongoing research as reported by the principal investigators at the second annual AESA Program meeting in May 1992: Laboratory studies are probing the mechanism responsible for many of the heterogeneous reactions that occur on stratospheric particles. Understanding how the atmosphere redistributes aircraft exhaust is critical to our knowing where the perturbed air will go and for how long it will remain in the stratosphere. The assessment of fleet effects is dependent on the ability to develop scenarios which correctly simulate fleet operations

    Markov Process of Muscle Motors

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    We study a Markov random process describing a muscle molecular motor behavior. Every motor is either bound up with a thin filament or unbound. In the bound state the motor creates a force proportional to its displacement from the neutral position. In both states the motor spend an exponential time depending on the state. The thin filament moves at its velocity proportional to average of all displacements of all motors. We assume that the time which a motor stays at the bound state does not depend on its displacement. Then one can find an exact solution of a non-linear equation appearing in the limit of infinite number of the motors.Comment: 10 page

    Heat transport measurements in turbulent rotating Rayleigh-Benard convection

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    We present experimental heat transport measurements of turbulent Rayleigh-B\'{e}nard convection with rotation about a vertical axis. The fluid, water with Prandtl number (σ\sigma) about 6, was confined in a cell which had a square cross section of 7.3 cm×\times7.3 cm and a height of 9.4 cm. Heat transport was measured for Rayleigh numbers 2×105<2\times 10^5 < Ra <5×108 < 5\times 10^8 and Taylor numbers 0<0 < Ta <5×109< 5\times 10^{9}. We show the variation of normalized heat transport, the Nusselt number, at fixed dimensional rotation rate ΩD\Omega_D, at fixed Ra varying Ta, at fixed Ta varying Ra, and at fixed Rossby number Ro. The scaling of heat transport in the range 10710^7 to about 10910^9 is roughly 0.29 with a Ro dependent coefficient or equivalently is also well fit by a combination of power laws of the form aRa1/5+bRa1/3a Ra^{1/5} + b Ra^{1/3}. The range of Ra is not sufficient to differentiate single power law or combined power law scaling. The overall impact of rotation on heat transport in turbulent convection is assessed.Comment: 16 pages, 12 figure

    Pink Sunshine

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    Untitled

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    Oh, Saturn

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    Starless Nights

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    Claire

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