2014
DOI: 10.1002/2013jd021243
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Physical simulation of atmospheric microbursts

Abstract: A laboratory simulation of atmospheric microbursts is presented. The physical model of the atmospheric phenomenon is reproduced at a reduced scale in a rotating tank (TURLab, Italy), the similitude is based on the Froude number. Different experiments were carried out varying the Rossby number, and the analysis of four significant cases is presented. The velocity, vorticity, and turbulent kinetic energy fields are evaluated together with the swirling strength analysis. The comparison with the natural prototype … Show more

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Cited by 3 publications
(2 citation statements)
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“…Atlas et al () use Doppler radar observations to conclude the concurrence with Srivastava's models and that a narrow distribution of hail meteor sizes produces stronger high‐reflectivity microbursts. Ferrero et al () perform laboratory simulations of microbursts to conclude that the fluid column height and density do not produce remarkable differences to the microburst, although high flow rotation can prevent the event, in contrast to former results. Pryor () produces the Microburst Windspeed Potential Index as a nowcasting algorithm.…”
Section: State Of the Artmentioning
confidence: 99%
“…Atlas et al () use Doppler radar observations to conclude the concurrence with Srivastava's models and that a narrow distribution of hail meteor sizes produces stronger high‐reflectivity microbursts. Ferrero et al () perform laboratory simulations of microbursts to conclude that the fluid column height and density do not produce remarkable differences to the microburst, although high flow rotation can prevent the event, in contrast to former results. Pryor () produces the Microburst Windspeed Potential Index as a nowcasting algorithm.…”
Section: State Of the Artmentioning
confidence: 99%
“…Enhanced physical understanding of the microburst phenomenon has been provided by highresolution simulations (e.g., Proctor 1988, Orf et al 1996, Orf and Anderson 1999, Nicholls et al 1993, and laboratory studies (e.g., Ferrero et al 2014). Because of its importance to aviation, LLWS is routinely forecasted using the vector wind difference of wind between 2000 ft AGL (619.5 m) and the surface (e.g., NOAA NWS Instruction 10-813, 2016), although these forecasts are mainly driven by resolvable non-convective sources, e.g., frontal passages, lowlevel jets, lee side mountain effects, sea breeze fronts, etc.…”
Section: Integrated Systems A) Numerical Guidance Systems For Aviationmentioning
confidence: 99%