1982
DOI: 10.1007/bf00170990
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The stability and uniqueness of coronal loops

Abstract: A hydrodynamic model of high resolution is used to examine the stability of coronal loops to finite amplitude perturbations. The loop is heated by means of a low-amplitude energy input and its subsequent dynamic relaxation is followed.Firstly, the initial atmosphere is generated by solving the time independent form of the hydrodynamic equations. It is shown that the loop structure depends critically on the balance between the radiative losses and the quiescent heating at the base of the transition zone, i.e. o… Show more

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Cited by 15 publications
(10 citation statements)
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“…The smallest cell-width in both simulations is reached at about 120 s. In simulation A it is about 6 × 10 2 cm and in simulation B about 10 3 cm. According to Craig et al (1982), a heat flux on the order of 10 8 erg cm −2 s −1 carried by the transition region requires a resolution of less than 3 × 10 3 cm. In Fig. 2 the conducted heat flux peaks at just below 10 8 erg cm −2 s −1 .…”
Section: The Dynamical Evolution Of the Plasmamentioning
confidence: 99%
“…The smallest cell-width in both simulations is reached at about 120 s. In simulation A it is about 6 × 10 2 cm and in simulation B about 10 3 cm. According to Craig et al (1982), a heat flux on the order of 10 8 erg cm −2 s −1 carried by the transition region requires a resolution of less than 3 × 10 3 cm. In Fig. 2 the conducted heat flux peaks at just below 10 8 erg cm −2 s −1 .…”
Section: The Dynamical Evolution Of the Plasmamentioning
confidence: 99%
“…The treatment of shocks needs care, but is well understood. Despite early recognition of the problems (e.g., Craig et al 1982), the numerical treatment of thermal conduction, in particular the resolution of steep temperature gradients, remains a serious concern. This can be seen by considering a static equilibrium loop.…”
Section: Introductionmentioning
confidence: 99%
“…With a Lagrangian formalism, Craig et al (1982) show how a summit heat pulse raises the summit temperature and later (by evaporation) the summit density, after which both decline as the plasma drains back down. Antiochos S Sturrock (1982) suggest that supersonic downflows in the late phase could be driven by footpoint cooling.…”
Section: A Loop Hydrodynamicsmentioning
confidence: 99%