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Velocity profile of interplanetary coronal mass ejections beyond 1 AU

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dc.contributor.author Lara, A. en_US
dc.contributor.author Flandes, A. en_US
dc.contributor.author Borgazzi, A. en_US
dc.contributor.author SUBRAMANIAN, PRASAD en_US
dc.date.accessioned 2020-10-19T04:06:25Z
dc.date.available 2020-10-19T04:06:25Z
dc.date.issued 2011-12 en_US
dc.identifier.citation Journal of Geophysical Research-Space Physics, 116. en_US
dc.identifier.issn 2169-9380 en_US
dc.identifier.issn 2169-9402 en_US
dc.identifier.uri http://dr.iiserpune.ac.in:8080/xmlui/handle/123456789/5152
dc.identifier.uri https://doi.org/10.1029/2011JA016807 en_US
dc.description.abstract [1] We analyze the dynamics of interplanetary coronal mass ejections (ICMEs) through the interplanetary medium from the lower solar corona to ∼5.3 AU. Our analysis uses a one‐dimensional hydrodynamical model derived from the fluid equation of motion that considers an effective drag force under both the laminar and turbulent hypotheses (low and high Reynolds number, respectively). The model has three sets of input parameters. The first set is related to the ICME itself, i. e., initial speed and mass; the second set of parameters is related to the ambient solar wind: density and velocity; and the final set corresponds to the ambient solar wind–ICME interaction: an ICME expansion factor and a viscosity or drag parameter. We use this model to explain the radial dynamics of a particular ICME detected at three different locations: close to the Sun, where the ICME was ejected on 20 January 2004, and detected by the SOHO/LASCO coronagraphs; two days later, at Earth's L1 by the ACE spacecraft (∼1.0 AU), and finally, ∼14 days later, at ∼5.3 AU by the Ulysses spacecraft near Jupiter's orbit. The model is then compared to a general set of ICMEs data from Ulysses that cover distances from ∼1.3 AU to ∼5.3 AU. Our model successfully reproduces the dynamical behavior of ICMEs at distances near Earth's orbit and works reasonably well at larger distances ≈5.3 AU. Therefore, our analysis shows that the ICME ‐ solar wind interaction may be treated as a drag interaction with the appropriate drag factors, not only at distances ≤1 AU, but at larger distances. Finally, we show that our model is useful in identifying ICMEs at different heliocentric distances. en_US
dc.language.iso en en_US
dc.publisher Wiley en_US
dc.subject Aerodynamic Drag en_US
dc.subject Acceleration en_US
dc.subject Dynamics en_US
dc.subject Images en_US
dc.subject 2011 en_US
dc.title Velocity profile of interplanetary coronal mass ejections beyond 1 AU en_US
dc.type Article en_US
dc.contributor.department Dept. of Physics en_US
dc.identifier.sourcetitle Journal of Geophysical Research-Space Physics en_US
dc.publication.originofpublisher Foreign en_US


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