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Siphon flows in isolated magnetic flux tubes. 3: The equilibrium path of the flux tube archThe arched equilibrium path of a thin magnetic flux tube in a plane-stratified, nonmagnetic atmosphere is calculated for cases in which the flux tube contains a steady siphon flow. The large scale mechanical equilibrium of the flux tube involves a balance among the magnetic buoyancy force, the net magnetic tension force due to the curvature of the flux tube axis, and the inertial (centrifugal) force due to the siphon flow along curved streamlines. The ends of the flux tube are assumed to be pinned down by some other external force. Both isothermal and adiabatic siphon flows are considered for flux tubes in an isothermal external atmosphere. For the isothermal case, in the absence of a siphon flow the equilibrium path reduces to the static arch calculated by Parker (1975, 1979). The presence of a siphon flow causes the flux tube arch to bend more sharply, so that magnetic tension can overcome the additional straightening effect of the inertial force, and reduces the maximum width of the arch. The curvature of the arch increases as the siphon flow speed increases. For a critical siphon flow, with supercritical flow in the downstream leg, the arch is asymmetric, with greater curvature in the downstream leg of the arch. Adiabatic flow have qualitatively similar effects, except that adiabatic cooling reduces the buoyancy of the flux tube and thus leads to significantly wider arches. In some cases the cooling is strong enough to create negative buoyancy along sections of the flux tube, requiring upward curvature of the flux tube path along these sections and sometimes leading to unusual equilibrium paths of periodic, sinusoidal form.
Document ID
19900010497
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Thomas, John H.
(Rochester Univ. NY., United States)
Montesinis, Benjamin
(Oxford Univ.)
Date Acquired
September 6, 2013
Publication Date
September 21, 1989
Subject Category
Physics (General)
Report/Patent Number
NASA-CR-186297
NAS 1.26:186297
Report Number: NASA-CR-186297
Report Number: NAS 1.26:186297
Accession Number
90N19813
Funding Number(s)
CONTRACT_GRANT: NAG5-934
CONTRACT_GRANT: NSG-7562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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