19,063 research outputs found

    A 'p-n' diode with hole and electron-doped lanthanum manganite

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    The hole-doped manganite La0.7Ca0.3MnO3 and the electron-doped manganite La0.7Ce0.3MnO3 undergo an insulator to metal transition at around 250 K, above which both behave as a polaronic semiconductor. We have successfully fabricated an epitaxial trilayer (La0.7Ca0.3MnO3/SrTiO3/La0.7Ce0.3MnO3), where SrTiO3 is an insulator. At room temperature, i.e. in the semiconducting regime, it exhibits asymmetric current-voltage (I-V) characteristics akin to a p-n diode. The observed asymmetry in the I-V characteristics disappears at low temperatures where both the manganite layers are metallic. To the best of our knowledge, this is the first report of such a p-n diode, using the polaronic semiconducting regime of doped manganites.Comment: PostScript text and 2 figures, to be published in Appl. Phys. Lett

    Wake Geometry Effects on Rotor Blade-Vortex Interaction Noise Directivity

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    Acoustic measurements from a model rotor wind tunnel test are presented which show that the directionality of rotor blade vortex interaction (BVI) noise is strongly dependent on the rotor advance ratio and disk attitude. A rotor free wake analysis is used to show that the general locus of interactions on the rotor disk is also strongly dependent on advance ratio and disk attitude. A comparison of the changing directionality of the BVI noise with changes in the interaction locations shows that the strongest noise radiation occurs in the direction of motion normal to the blade span at the time of interaction, for both advancing and retreating side BVI. For advancing side interactions, the BVI radiation angle down from the tip-path plane appears relatively insensitive to rotor operating condition and is typically between 40 and 55 deg below the disk. However, the azimuthal radiation direction shows a clear trend with descent speed, moving towards the right of the flight path with increasing descent speed. The movement of the strongest radiation direction is attributed to the movement of the interaction locations on the rotor disk with increasing descent speed

    Target support for inertial confinement fusion

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    Advancing-side directivity and retreating-side interactions of model rotor blade-vortex interaction noise

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    Acoustic data are presented from a 40 percent scale model of the four-bladed BO-105 helicopter main rotor, tested in a large aerodynamic wind tunnel. Rotor blade-vortex interaction (BVI) noise data in the low-speed flight range were acquired using a traversing in-flow microphone array. Acoustic results presented are used to assess the acoustic far field of BVI noise, to map the directivity and temporal characteristics of BVI impulsive noise, and to show the existence of retreating-side BVI signals. The characterics of the acoustic radiation patterns, which can often be strongly focused, are found to be very dependent on rotor operating condition. The acoustic signals exhibit multiple blade-vortex interactions per blade with broad impulsive content at lower speeds, while at higher speeds, they exhibit fewer interactions per blade, with much sharper, higher amplitude acoustic signals. Moderate-amplitude BVI acoustic signals measured under the aft retreating quadrant of the rotor are shown to originate from the retreating side of the rotor

    Helicopter model rotor-blade vortex interaction impulsive noise: Scalability and parametric variations

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    Acoustic data taken in the anechoic Deutsch-Niederlaendischer Windkanal (DNW) have documented the blade vortex interaction (BVI) impulsive noise radiated from a 1/7-scale model main rotor of the AH-1 series helicopter. Averaged model scale data were compared with averaged full scale, inflight acoustic data under similar nondimensional test conditions. At low advance ratios (mu = 0.164 to 0.194), the data scale remarkable well in level and waveform shape, and also duplicate the directivity pattern of BVI impulsive noise. At moderate advance ratios (mu = 0.224 to 0.270), the scaling deteriorates, suggesting that the model scale rotor is not adequately simulating the full scale BVI noise; presently, no proved explanation of this discrepancy exists. Carefully performed parametric variations over a complete matrix of testing conditions have shown that all of the four governing nondimensional parameters - tip Mach number at hover, advance ratio, local inflow ratio, and thrust coefficient - are highly sensitive to BVI noise radiation

    Model helicopter rotor high-speed impulsive noise: Measured acoustics and blade pressures

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    A 1/17-scale research model of the AH-1 series helicopter main rotor was tested. Model-rotor acoustic and simultaneous blade pressure data were recorded at high speeds where full-scale helicopter high-speed impulsive noise levels are known to be dominant. Model-rotor measurements of the peak acoustic pressure levels, waveform shapes, and directively patterns are directly compared with full-scale investigations, using an equivalent in-flight technique. Model acoustic data are shown to scale remarkably well in shape and in amplitude with full-scale results. Model rotor-blade pressures are presented for rotor operating conditions both with and without shock-like discontinuities in the radiated acoustic waveform. Acoustically, both model and full-scale measurements support current evidence that above certain high subsonic advancing-tip Mach numbers, local shock waves that exist on the rotor blades ""delocalize'' and radiate to the acoustic far-field

    Light interception, gas exchange and carbon balance of different canopy zones of minimally and cane-pruned field-grown Riesling grapevines

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    Leaf area development, pre-dawn leaf water potential, spatial and temporal patterns of light interception and photosynthesis (A) of minimal pruned (MP) and cane-pruned vertical shoot positioned (VSP) fieldgrown Riesling grapevines were monitored in 2002 and 2003. In order to quantify the contribution of different canopy segments to whole vine carbon gain, diurnal single leaf gas exchange measurements were conducted several times during the season in 8 different canopy segments keeping leaves in their natural position. Carbon losses due to nocturnal respiration (DR) were estimated with a model describing the dependence of DR on temperature. MP vines had about 17 times more but less vigorous shoots with smaller leaves. Leaf area (LA) development was faster for MP than for VSP vines and LA was 2.5-3-fold higher for most of the season. Spatial and temporal patterns of average daily light interception were related to LA development and canopy dimensions for both MP and VSP vines during the first part of the season, but increased independent of LA until mid-October and more so for VSP than MP. Diurnal gas exchange measurements showed differences between canopy segments, measuring dates and systems. Differences between segments were related to light interception in the absence of water deficit, high leaf temperature and vapour pressure deficit. The higher light interception of MP vines caused pre-dawn water potential to decrease faster and to remain at lower levels during most of the season. This limited A more severely for leaves of MP vines in canopy segments which were well exposed to light. The estimated seasonal carbon gain per canopy segment was highest in the apical canopy zones for both canopy systems but carbon assimilation was higher for MP than for VSP vines in all segments with the exception of the interior canopy. Respiratory losses by leaves depended on night temperature and time during the season but generally varied between 3 and 7 % of the amount of carbon gained during the day. MP vines had slightly higher relative respiration losses than VSP vines. On a whole-plant basis, carbon gain of MP vines was between 5.7 (beginning of the season) and 2.2 times (end of season) higher than for VSP vines.

    Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch Wind Tunnel (DNW)

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    Acoustic data are presented from a 40 percent scale model of the 4-bladed BO-105 helicopter main rotor, measured in the large European aeroacoustic wind tunnel, the DNW. Rotor blade-vortex interaction (BVI) noise data in the low speed flight range were acquired using a traversing in-flow microphone array. The experimental apparatus, testing procedures, calibration results, and experimental objectives are fully described. A large representative set of averaged acoustic signals is presented

    Electron Impact Ionization Close to the Threshold: Classical Calculations

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    In this paper we present Classical Trajectory Monte Carlo (CTMC) calculations for single and multiple electron ionization of Argon atoms and ions in the threshold region. We are able to recover the Wannier exponents a for the power-law behavior of the cross section s versus excess energy: the exact value of the exponent as well as the existence of its saturation for multiple ionization appear to be related to how the total binding energy is shared between target electrons.Comment: 9 pages. To be published in Journal of Physics
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