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contributor authorXia, J.
contributor authorLewellen, W. S.
contributor authorLewellen, D. C.
date accessioned2017-06-09T14:38:25Z
date available2017-06-09T14:38:25Z
date copyright2003/11/01
date issued2003
identifier issn0022-4928
identifier otherams-23364.pdf
identifier urihttp://onlinelibrary.yabesh.ir/handle/yetl/4159917
description abstractSince maximum Mach numbers in an F5 tornado are expected to, at least, reach ?0.4, a study was undertaken to determine the major potential compressibility effects in such flows. Results from compressible large-eddy simulations of tornado corner flow dynamics are summarized. Comparison with previous incompressible simulations indicates that Mach number effects tend to be modest and may be estimated by an isentropic approximation. As the average maximum Mach number M within the tornado increases above one-half, the largest changes occur for ?low-swirl? corner flows, those exhibiting a central vertical jet off the surface capped by a vortex breakdown, with the vortex breakdown found to occur at significantly greater heights as M increases. It also appears that the highest Mach numbers are most likely to occur during rapid transients in near-surface intensification that can sometimes occur during a tornado's evolution.
publisherAmerican Meteorological Society
titleInfluence of Mach Number on Tornado Corner Flow Dynamics
typeJournal Paper
journal volume60
journal issue22
journal titleJournal of the Atmospheric Sciences
identifier doi10.1175/1520-0469(2003)060<2820:IOMNOT>2.0.CO;2
journal fristpage2820
journal lastpage2825
treeJournal of the Atmospheric Sciences:;2003:;Volume( 060 ):;issue: 022
contenttypeFulltext


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