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  • 1
    Publication Date: 2014-10-01
    Description: The replacement of native C 4 -dominated grassland by C 3 -dominated shrubland is considered an ecological state transition where different ecological communities can exist under similar environmental conditions. These state transitions are occurring globally, and may be exacerbated by climate change. One consequence of the global increase in woody vegetation may be enhanced ecosystem carbon sequestration, although the responses of arid and semiarid ecosystems may be highly variable. During a drier than average period from 2007-2011 in the northern Chihuahuan Desert, we found established shrubland to sequester 49 g C m −2 year −1 on average, while nearby native C 4 grassland was a net source of 31 g C m −2 year −1 over this same period. Differences in C exchange between these ecosystems were pronounced - grassland had similar productivity compared to shrubland but experienced higher C efflux via ecosystem respiration, while shrubland was a consistent C sink because of a longer growing season and lower ecosystem respiration. At daily timescales, rates of carbon exchange were more sensitive to soil moisture variation in grassland than shrubland, such that grassland had a net uptake of C when wet but lost C when dry. Thus, even under unfavorable, drier than average climate conditions, the state transition from grassland to shrubland resulted in a substantial increase in terrestrial C sequestration. These results illustrate the inherent tradeoffs in quantifying ecosystem services that result from ecological state transitions, such as shrub encroachment. In this case, the deleterious changes to ecosystem services often linked to grassland to shrubland state transitions may at least be partially offset by increased ecosystem carbon sequestration. This article is protected by copyright. All rights reserved.
    Print ISSN: 1354-1013
    Electronic ISSN: 1365-2486
    Topics: Biology , Energy, Environment Protection, Nuclear Power Engineering , Geography
    Published by Wiley
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  • 2
    Publication Date: 1963-01-01
    Print ISSN: 0031-9171
    Topics: Physics
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  • 3
    Publication Date: 2019-06-28
    Description: An experimental study of several of the trailing edge and wake turbulence properties for a NACA 64A010 airfoil section was completed. The experiment was conducted at the Ohio State University Aeronautical and Astronautical Research Laboratory in the 6 inch X 22 inch transonic wind tunnel facility. The data were obtained at a free stream Mach number of 0.80 and a flow Reynolds number (based on chord length) of 5 million. The principle diagnostic tool was a dual-component laser Doppler velocimeter. The experimental data included surface static pressures, chordwise and vertical mean velocities, RMS turbulence intensities, local flow angles, and a determination of turbulence kinetic energy in the wake. Two angles of attack (0 and 2 degrees) were investigated. At these incidence angles, four flow field surveys were obtained ranging in position from the surface of the airfoil, between the transonic shock and the trailing edge, to the far-wake. At both angles of attack, the turbulence intensities and turbulence kinetic energy were observed to decay in the streamwise direction. In the far wake, for the non-lifting case, the turbulence intensities were nearly isotropic. For the two degree case, the horizontal component of the turbulence intensity was observed to be substantially higher than the vertical component.
    Keywords: AERODYNAMICS
    Type: NASA-CR-176904 , NAS 1.26:176904
    Format: application/pdf
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  • 4
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    Publication Date: 2019-06-28
    Description: An experimental study of several of the trailing edge and wake turbulence properties for a NACA 64A010 airfoil section was completed. The experiments were conducted at the Ohio State University Aeronautical and Astronautical Research Laboratory in the 6 inch x 22 inch transonic wind tunnel facility. The data were obtained at a free stream Mach number of 0.80 and a flow Reynolds number (based on chord length) of 5 million. The principal diagnostic tool was a dual-component laser Doppler velocimeter. The experimental data included surface static pressures, chordwise and vertical mean velocities, RMS turbulence intensities, local flow angles, and a determination of turbulence kinetic energy in the wake at chordwise locations between the transonic shock wave and the trailing edge, in the near wake just downstream of the trailing edge and in the far wake. At the two angles of attack tested (0 and 2 degrees), the turbulence intensities and turbulence kinetic energy were observed to decay in the streamwise direction. In the far wake, for the non-lifting case, the turbulence intensities were nearly isotropic. For the two degree case, the horizontal component of the turbulence intensity was observed to be substantially higher than the vertical component.
    Keywords: AERODYNAMICS
    Format: text
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  • 5
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    Publication Date: 2019-05-30
    Description: Electron beam density measurements, discussing effect of elevated rotational and vibrational temperatures
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: AIAA JOURNAL
    Format: text
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  • 6
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    Publication Date: 2019-05-30
    Description: Spectroscopic electron beam diagnostic technique, examining negligible effect elevated vibrational temperatures have on measured rotational temperatures of molecular nitrogen
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: AIAA PAPER 66-747
    Format: text
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  • 7
    Publication Date: 2019-06-28
    Description: Preliminary design methods are presented for vehicle aerothermodynamics. Predictions are made for Shuttle orbiter, a Mach 6 transport vehicle and a high-speed missile configuration. Rapid and accurate methods are discussed for obtaining aerodynamic coefficients and heat transfer rates for laminar and turbulent flows for vehicles at high angles of attack and hypersonic Mach numbers.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 87-2545
    Format: text
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  • 8
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    Publication Date: 2019-06-27
    Description: Boundary layer in nozzle of arc-heated wind tunnel, obtaining velocity, temperature and density profiles
    Keywords: FLUID MECHANICS
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  • 9
    Publication Date: 2019-06-27
    Description: Experimental and theoretical analyses of high speed laminar boundary layer in nozzle of arc heated wind tunnel
    Keywords: FLUID MECHANICS
    Type: NASA-CR-96152 , REPT.-5
    Format: application/pdf
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  • 10
    Publication Date: 2019-07-13
    Description: In the present comparative study of computer codes for the modeling of two-dimensional, single element airfoil sections for various section geometry classes, two of the codes use vortex singularities methods to obtain the potential flow solution while the remainder solve the full inviscid potential flow equations by means of finite differencing techniques that allow results to be obtained for transonic flow about an airfoil which includes weak shocks. Computational results are presented for a symmetrical airfoil section, a conventional section, and a supercritical one. Icing condition applications of the models are noted. The model codes' range of applicability and agreement with each other and experimental results, as well as their computer run times and memory requirements, are noted.
    Keywords: AERODYNAMICS
    Type: Aerospace simulation; Feb 02, 1984 - Feb 04, 1984; San Diego, CA
    Format: text
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