Dynamic 3D reconnection in a separator geometry with two null points

Size: px
Start display at page:

Download "Dynamic 3D reconnection in a separator geometry with two null points"

Transcription

1 Dnamic 3D reconnection in a separator geometr with two null points D. I. Pontin 1 & I. J. D. Craig Department of Mathematics, Universit of Waikato, Private Bag 35, Hamilton, New Zealand. ABSTRACT The dnamic behaviour of disturbances in the vicinit of a pair of magneticall connected 3D null points is eamined. The aim is to investigate how nonlinear disturbances lead to strong localized currents that initiate magnetic reconnection at the separator. The problem is formulated in an incompressible clindrical geometer b superposing arbitrar disturbance fields onto a background two-null field. Two different regimes are found for the dnamic evolution, depending on the relative strengths of the background magnetic and velocit fields. In one regime, disturbance pulses split into ingoing and outgoing components, which propagate along the background field lines. In the other flu pile-up regime, a strong driving flow localises the disturbances towards the null point pair. Current structures aligned with the spines, fans and separator present in the field are found to result, and the structure of these currents and their scaling with resistivit is investigated. Subject headings: MHD plasmas Sun: flares Sun: magnetic fields 1. Introduction Magnetic reconnection is a process which is fundamental to man phenomena in astrophsical and laborator plasmas. Reconnection is the onl mechanism capable of releasing topologicall bound magnetic energ, in the form of Ohmic heating and the kinetic energ of mass motion. Most astrophsical plasmas, however, are highl conducting the dimensionless collisional resistivit is an inverse Lundquist number of order η and for reconnection to be effective, localized regions comprising huge magnetic field gradients, and 1 Present address: Space Science Center, Universit of New Hampshire, Durham NH3, USA.

2 therefore strong currents, must be present. In this paper, we will investigate the growth of such intense currents in a magnetic separator topolog. We concentrate here on magnetic reconnection in the presence of 3D null points of the magnetic field. The resulting spine and fan separatri topolog of the background field will be outlined in the following section. For the present, we emphasize that reconnection at separatri surfaces, as well as at separator lines linking the nulls, is thought to be important in both solar and stellar atmospheres, as well as closer to home in the Earth s magnetosphere. In the solar corona in particular, it is predicted that there should be present an abundance of 3D null points (e.g. Inverarit and Priest 1999; Albright 1999; Longcope et al. 3) and separators (Schrijver and Title ; Beveridge and Longcope 5). It is further predicted that such sites should provide priviliged regions for heating the corona (Longcope 199; Antiochos et al. ; Priest et al. 5). There is also observational evidence that reconnection at a 3D null point ma act as a trigger for some solar flares (Fletcher et al. 1). Our present aim is to stud separator reconnection. Despite being invoked as an eplanation for man dnamic phenomena in the corona, such as X-ra bright points (Longcope et al. 1) and solar flares (Longcope and Noonan ), the mechanisms of separator reconnection are not well understood. What is known is that separator reconnection occurs quite naturall on the Sun, for eample, when two photospheric flu sources move relative to one another in the presence of an overling field (Parnell and Galsgaard ). Observational evidence of separator reconnection in the corona has recentl been presented b Longcope et al. (5). In addition, it has been shown that flare statistics can be modelled using a superposition of separators (Wheatland ). In this paper, we develop solutions which model current growth and reconnection at a separator. Due to the etremel low value of the resistivit in astrophsical plasmas, a crucial propert of an reconnection model is the predicted reconnection rate, and whether it is sufficient to eplain observed dnamic phenomena at realistic plasma parameters. To this end, we will discuss the scaling properties of the peak current with resistivit in each of the regimes described. The model is based upon the principles first developed b Craig and Henton (1995), who proposed a stead-state, resistive, planar model for reconnection at a two-dimensional (D) null point. This work has since been generalised into three dimensions, firstl with the addition of an aial field to the D X-point, such that there is no null in the field (Craig et al. 1995), and secondl to spine and fan reconnection at single 3D nulls (Craig and Fabling 199). Further generalisations are possible to include the effects of timedependence (Craig and Fabling 199), as well as additional (non-resistive) non-ideal effects (e.g. Ji and Song 1; Craig and Watson 3). In what follows we develop a resistive, time-dependent model for reconnection occurring

3 3 in a magnetic field in clindrical geometr, where either one or two 3D null points are present. This etends and generalises the work of Watson and Craig (), who made a preliminar investigation of similar configurations in a stead-state regime (see also Tassi et al. 3), and provides the possibilit of reconnection at curved current sheets and also separator current sheets. Although we consider here onl resistive non-ideal effects, we do not epect that the introduction of further non-ideal effects would alter the qualitative results significantl. Hall currents, for eample, are capable of having a profound effect on the detailed microphsics of the reconnection region. Their effect depends, however, both on the smmetries of the reconnection problem, and on the presence of background guide fields (Craig and Watson 3, 5). For the present, we simplif our discussion b concentrating on the buildup of strong field gradients in the vicinit of the reconnection region. In Section we discuss the topolog of the magnetic fields considered. In Section 3 we introduce the governing MHD equations and describe the method of analsis, emphasising in particular the wave properties of the solution, which we believe provide generic signatures for all transient magnetic merging solutions. In Sections and 5 the results of numerical simulations of the equations are discussed and their scalings with resistivit are summarized. We present our conclusions in Section.. Topolog of connected null point pairs We begin b summarizing the magnetic field topolog associated with 3D nulls. The field lines which asmptoticall approach 3D null points provide a local skeleton of the magnetic field. In the case of a single 3D null the skeleton comprises a spine line and a fan surface. The spine is a pair of field lines which approach (recede from) the null in opposite directions, while a famil of field lines radiate out from (into) the null in the fan plane (e.g. Fukao et al. 1975; Lau and Finn 199; Parnell et al. 199). B considering a Talor epansion of B about the null point, it can be seen that the orientation of the spine and fan are determined b the eigenvectors of the matri B. This matri is traceless, and the eigenvectors corresponding to the eigenvalues of like sign (or whose real parts have like sign) determine the orientation of the fan, while the other defines the spine. In general, the field strength in the fan will not be isotropic, and this anisotrop is determined b the fan eigenvalues. When two null points are present a separator a field line which directl connects the nulls ma eist. Kinematic considerations for fields containing multiple nulls (Lau and Finn 199; Priest and Titov 199) suggest that spines, fans and separators provide special sites at which magnetic reconnection can occur, and this view has been well supported b stead state reconnection solutions (Craig et al. 1999).

4 In what follows we consider a two-null field whose separator is formed b the intersecting fan planes of the component nulls. This structure provides a generic separator geometr in the sense that the separator line is topologicall stable, being robust to arbitrar, small perturbations in the background field. Note that, although a separator could be formed b the coeistence of two null spines or one spine and one fan field line, neither of these structures is topologicall stable, due to the uniqueness of the spine lines. This is one advantage of the present stud over that of Craig et al. (1999), who consider a general class of fields containing multiple nulls in a stead-state regime. In this case spine-fan separators are present, which can onl be maintained b the high degree of smmetr present in the field. We believe the geometr of the present stud also provides a significant improvement on man previous studies of separator reconnection, which model the separator simpl using a planar X-point threaded b an arbitrar aial field (e.g. Heerikhuisen and Craig ). As we will show, the influence of the nulls themselves cannot be discounted when considering separator reconnection. 3. The MHD equations 3.1. Form of the solution We assume the equations of collisional resistive MHD, based on an incompressible plasma in an open (unbounded) geometr. The problem is scaled according to the reference coronal values B c = G, l c = 9.5 cm, n c = 9 cm 3, v A = 9 cm s 1. Time is now measured in units of the Alfvén time τ A = l c /v A, which is tpicall a few seconds in coronal applications. In this formulation the plasma resistivit is an inverse Lundquist number η 1. The simplifing assumption will be made that the viscosit ν is isotropic. In the simulations described later, ν is chosen to scale linearl with η this choice has been shown to reproduce the pure resistive scalings of the current laer (Craig and Watson 5). The dimensionless induction equation is given b B t = (V B) + η B, (1) while taking the curl of the viscous momentum equation we obtain Ω t = (J B) (Ω V) + ν Ω, ()

5 5 where J = B is the current, Ω = V is the vorticit, and η and ν are assumed constant. We must also impose the constraint equations B =, V =. (3) Once the magnetic and velocit fields have been found, the plasma pressure ma be obtained from the uncurled form of the momentum equation. The assumption of an incompressible plasma ( V = ) is made in order to facilitate our method of solution, since in this form the equations displa a high degree of smmetr between B and V (Craig and Henton 1995). Furthermore, once the current sheet has formed, its behaviour is epected to be largel incompressible, as the global timescale for merging is tpicall much longer than the timescale for fast mode propagation across the current sheet. It has been shown that finite compressibilit has onl a weak effect on the scaling properties of flu pile-up current sheets, and in fact acts to marginall speed up the resultant reconnection (see Litvinenko and Craig 3, and references therein). In order to construct reconnection solutions, we use the superposition technique of Craig and Henton (1995), and let B = βp() + b(, t), V = αp() + v(, t), () where P is a stead-state potential background field, and b and v are disturbance fields of arbitrar amplitude. The method of solution is based on choosing a form of reduced dimensionalit for the disturbance fields such that Equations (1) and () ma be reduced to a sstem of ordinar differential equations. In the stead-state regime, this corresponds to automaticall satisfing the momentum equation, leaving onl the induction equation to be solved. In this case, v() = (β/α)b(), and in order for the momentum equation to be automaticall satisfied we require (( b) b) =. (5) In previous models based on Cartesian geometr b has taken either the form b = f(, )ẑ or b = f()ŷ +g()ẑ (or cclic permutations thereof). It is interesting to note that these forms are in fact over-restrictive for this method, in that the satisf ( b) b =, whereas this quantit need onl be curl-free. In clindrical coordinates we find that there is a reduced choice of such low-dimensionalit disturbances. Of those forms which satisf the divergence condition, the onl two which additionall satisf (5) are b 1 = b(r, θ, t)ẑ, b = a(r, t)ˆθ + b(r, t)ẑ. ()

6 In contrast to the Cartesian case, these forms do not satisf the more restrictive condition ( b) b =. The disturbance form of most interest to us is b 1, since the second form describes disturbance field structures which var onl in the radial direction. Disturbances based on b 1 provide a richer structure to the resulting currents, and can in an case be used to model a single component of the form b b turning off the θ-dependence. Guided b the above considerations, we take B = βp + b(r, θ, t)ẑ, V = αp + v(r, θ, t)ẑ. (7) B analog with the Cartesian case, we look for a potential field P = (P 1 (r), P (r, θ), P 3 (r, z)) which is linear in θ and z. The onl potential field of this form is ( { γln(r/l) P = + κr } γθ, (r/l) l (r/l), κz ), () l where γ, κ and l are constants. We note that the field is singular at the origin, and nonperiodic in θ, and so the solution ma not be considered as global, but rather must be considered valid onl in some restricted annular domain which ecludes the origin and the negative -ais (θ = ±π). The background field P ma contain one or two null points, depending on the values of γ and κ, while l is a scale factor which determines the distance of the null point pair from the origin. If γ and κ are of the same sign, then onl a single null is present, however if γ and κ are of opposite sign and γ > κ e then two nulls are present. The skeleton of the field in each case is shown in Figure 1. Here we will concentrate primaril on the case where two nulls are present in the field. As shown in the figure, the nulls are joined b a separator (along θ = z = ), formed b the intersection of their fan planes. 3.. Equations for the disturbance fields Substituting the above epressions for B and V (Eqs. (7) and ()), into Equations (1) and (), we find that ( κ ) ( κ ) b t = α l L b β l L v + η b (9) ( κ ) ( κ ) v t = α l + L v + β l + L b + ν v + g(t) () where L = P 1 r + P { γl ln(r/l) r θ = + κr } r + γlθ r l r θ (11)

7 7 is the directional derivative along P in the rθ-plane, and a = (1/r) (ra r ) r + (1/r )a θθ, (1) and where subscripted letters denote partial derivatives. Equation () is obtained b integrating either component of () emploing integration b parts, with the arbitrar function of time g(t) being the constant of integration. Note that g simpl gives a time-varing but spatiall uniform z-component of V, that is a uniform shift of the flow structure in the z-direction. Thus, in order to maintain the co-spatial nature of the null points of the background magnetic and flow fields, we hereafter set g =. A procedure analogous to that described above can be used to derive the corresponding equations when the disturbance field takes the form b in Equation (), as described in Appendi A Wave properties of the solution In the majorit of astrophsical plasmas, non-ideal effects onl become important when ver small length scales develop, due to the fact that the resistive and viscous coefficients (η and ν) are so small. It is therefore natural to eamine the properties of our sstem in the ideal limit, when η = ν =. This problem is simplified b invoking the Elsasser variables M = b v and N = b + v, which from (9) and () satisf M t = (α β) κ N (α + β)lm, (13) l N t = (α + β) κ M (α β)ln. (1) l To simplif further, observe that the operator L must be epressible as a total derivative since it defines the directional derivative along the background planar field. More formall, we can change from the (r, θ) coordinates to a sstem (ψ, χ) based on the (planar projected) field lines dr = rdθ, (15) P 1 P which are labelled b ψ. It follows that χ is a coordinate running along the field lines, such that ψ χ. B a suitable choice we can make the directional derivative L χ. The further change to a comoving frame τ = t, s = χ αt reduces sstem (13,1) to M τ = (α β) κ l N βm s, (1) N τ = (α + β) κ l M + βn s. (17)

8 It follows from this that both M and N, and thus b and v, satisf the generalised Klein- Gordon equation b ττ = β b ss + κ l (α β )b. (1) This equation for the disturbance field highlights the wave-like nature of the problem. First note that Equation (1) has two characteristics, C ± = s ± βτ = χ (α β)τ. (19) Obviousl, if α > β, then both characteristics correspond to waves propagating along the field lines in the positive χ direction, of different speeds. B contrast, if α < β, then the characteristics correspond to two waves which propagate in opposite directions (see also Craig and Fabling 199). Thus, there are two different possible regimes for the solution, depending on the relative sizes of α and β. The waves are Alfvén waves, which represent the incompressible limit of (compressive) fast-mode Alfvénic disturbances. A further ke propert is the possibilit of growth in the solution. Obviousl growth, as opposed to oscillator behaviour, can occur onl if the source term of (1) is positive, that is, α > β. Note that Equation (1) is a generalization of the Cartesian fan equation analzed b Craig and Fabling (199) using Fourier transform methods. Appling their analsis to (1) suggests that the condition for growth derived above ma be sufficient, even when small dissipation coefficients are accounted for. In an case, growth depends not onl on a sufficientl strong driving flow, but also on the sign of the parameter κ of the background field. In order to obtain growth, we require in addition that the background flow has the capacit to stretch and amplif the disturbance field, bẑ. For this reason, we will concentrate on the case κ >. 3.. Numerical simulations We now consider numerical simulations of Equations (9) and () based on a purpose built, predictor-corrector scheme on a clindrical mesh. In all cases the potential background fields are perturbed b imposing a single initial magnetic field pulse (b) at some location within the numerical domain. We first concentrate on two-null oscillator β > α solutions, before going on to discuss flu pile-up models. In all of the simulations we take ν = η, since a linear scaling of ν with η is known to preserve the purel resistive scalings (Craig and Watson 5). Note also that we find that the chosen value of ν has little effect on the results discussed.

9 9. Wave-like regime ( β > α ) According to the previous analsis, when the background magnetic field dominates the driving flow the evolution of the disturbance field is characterised b inward and outward propagating waves. Thus the initial disturbance is epected to spread along the background field lines, within an envelope bounded b peaks travelling in and moving out at speeds α ± β, as determined b (19). Figures (-) show that this behaviour is reproduced in the simulations (these figures show frames from animations, which can be viewed at math97/cl anim.html). We see that the magnetic disturbance develops two separate peaks, which travel along the field lines of P toward and awa from the null point pair. However, the geometr of the background field lines, and the location of the initial disturbance with respect to the background field structure, are found to influence, quite strongl, the localisation of the ingoing pulse. In the present simulations the direction of the magnetic field and plasma flow are quite arbitrar: the flow ma be in either direction, and although this influences the relative speeds of the peaks of the disturbance, the localisation and current growth properties remain unaffected. The background field structure is the two-null structure of Figure 1(b). There is one null, hereafter named null 1, whose fan lies in the rz-plane and whose curved spine lies in the rθ-plane; and another ( null ) whose fan lies in the rθ-plane and whose spine lies in the z-direction. The spine of each null bounds the fan surface of the other. If the initial pulse is located to the negative- side of the spine of null 1, or if it disturbs this spine, then the disturbance spreads out and localises to the fan of null 1, as shown Figure. However, if the disturbance is initiated in the fan of null (i.e. to the positive- side of the spine of null 1), then in general the ingoing pulse is squeezed in towards null along P, where it localises towards the spine, as in Figure 3. In addition, a third tpe of behaviour ma occur. If the disturbance is initiated in the fan of null, but sufficientl close to the spine of null 1, then the ingoing pulse will be transported inwards towards the separator joining the two nulls, as in Figure, the disturbance being aligned with the fan plane of null 1. The relative size of the region of space in which this separator localisation occurs depends on the geometr of the field lines in the fan of null, or equivalentl the isotrop of this null, since the disturbances propagate along P. In each of the three cases described above, the outgoing peak moves outwards along P, spreading due to diffusion and the increasing plasma velocit awa from the nulls. Of central interest, in each of the above cases, is whether a growth in the current densit occurs, and to what etent this depends on the resistivit η. As epected, the magnitude of both disturbance peaks decas in time, as there is no flu pile-up occurring. The current associated with the outgoing pulse does indeed deca, but the ingoing pulse is

10 alwas associated with current growth. The growth is stalled when resistive effects begin to dominate. Independent results for the advection of magnetic pulses suggest that, in the absence of flu pile-up, the peak current is controlled b the width η of the current laer (e.g. Craig and Fabling 199). This corresponds to a slow Sweet-Parker dissipation rate. We find here that, while this scaling is not adhered to strictl in the present more comple field structure, it is approimatel followed. Figure 5 shows a logarithmic plot of peak current versus resistivit for each of the spine, fan and separator cases. Thus if J ma follows a power-law dependence of the form J ma η µ J, () then the gradient determines µ J. Also plotted, for comparison, are the results for a similar run in which a localisation towards the curved fan plane of the single null field shown in Figure 1(a) was considered. The results are displaed in the top portion of Table 1. Note that while the fan current scaling is similar in the two cases considered, the spine and separator currents scale somewhat more slowl. These descrepancies can perhaps be attributed to the lack of highl localized current structures in the present clindrical geometr. In an case, since the scaling of the peak current with resistivit is such that the resulting reconnection rate is unlikel to be energeticall significant at realistic values of the resistivit, it seems more profitable to consider possible enhancements in the flu pile-up regime with α > β. 5. Flu pile-up regime ( α > β ) 5.1. Localisation phase We now eamine the evolution of our sstem in the regime α > β. Consider first the ideal limit with η = ν =. Since we require that our dnamic models must be able to reproduce the stead state solutions, in which v = (β/α)b, we introduce the function f = v (β/α)b to measure departures from the stead state. Now, rewriting Equations (9) and () in terms of b and f, we have in the ideal limit (η = ν = ) that b t + α Lb = κ ( κ ) l α b β l L f, (1) f t + α + Lf = α κ l f β α α ( κ l L ) b, () where α + = α + β α, α = α β. α

11 11 The advection terms on the left hand side of the above equations suggest that the field f evolves more quickl than b, as the coefficients α + and α determine inverse time-scales for these processes, and α + > α. If we now consider the limit of ver strong flow, that is β/α 1, and use the variable s to compute the directional derivative, so that Lf f s, then Equation () becomes f t + α + f s + α κ l f =, with solution ( ) f = f s e α+ t e α (κ/l)t. (3) Equation (3) demonstrates the spatial localisation of f along the background field lines, for α > corresponding to inflow in the rθ-plane, as well as indicating an eponential deca in time. Therefore, for large time we ma neglect f in the evolution equation for b. Setting f = in (1), we deduce, as above, that ( ) b = b s e α t e α (κ/l)t, () which shows a slower localisation of b than f, coupled with an eponential growth of b. We conclude that the immediate effect of the magnetic perturbation is to drive the velocit disturbance field towards its quasi-stead state distribution (v (β/α)b). Once the equilization phase has occurred, the disturbance fields begin a gradual localisation phase, which is accompanied b eponential growth. This growth is arrested once length scales are sufficientl reduced so that non-ideal effects become important. 5.. Simulation results We now summarize numerical simulations performed in the regime α > β. Once again, the initial conditions are chosen such that v = at t =, and b is some non-zero disturbance pulse. The earl phase of the evolution confirms that the velocit profile v does indeed quickl grow (to v (β/α)b), in order to mirror the magnetic disturbance field profile. Once this has happened, the behaviour of v closel follows that of b, with just a small phase dela. Both disturbance fields are then advected towards the null point pair, with the magnitude of the magnetic field disturbance, as well as the current, growing as the localisation proceeds. As described in Section, the nature of this localisation depends on the relationship between the initial disturbance and the background field P, and again localisation towards the spine, fan, or separator is possible in the double null field. In each case, we require α > to ensure inflow of the disturbances.

12 Fan reconnection We eamine first the case of fan reconnection. Consider first an isolated linear 3D background null, of the form Q = (λ 1, (λ λ 1 ), λ z), where λ > λ 1 >. In this case, the fan is the plane z =, and a tpical disturbance has - and -components, which are epected to scale with resistivit as J ma η µ J, B ma η µ b, (5) where µ J = (1 + A)/, µ b = A/ and A = λ 1 /λ (for the -component) or (λ λ 1 )/λ (-component) (see Craig and Fabling 199; Heerikhuisen and Craig ). Hence, when the null point is isotropic (λ 1 = λ /), each component is equall magnified (A = 1/). However, if the null is non-isotropic, and therefore the outflow in the fan is stronger in one direction (as defined b the eigensstem of the null see Section ), then one component will be stretched and magnified more strongl than the other. Our present purpose is to test whether the above scalings persist in more complicated field configurations for both the single and double null background fields. The disturbance field in our case is alwas aligned to the z-ais, and it is the background fan field that governs the strength of the outflow in this direction. Now, in order to determine the epected scalings (as predicted b the theor for a single linear null point), it is necessar to calculate the appropriate ratio of the eigenvalues of the matri B at the null (see Section ). As discussed above, this is the ratio of the outflow eigenvalue corresponding to the direction parallel to the disturbance component to the inflow eigenvalue. For the case of the single null background field, a curved current sheet is formed in the fan plane of the null (the zθ-plane). The peak current and maimum field at time of peak current are plotted in Figure (a). B comparison with the field Q, we see that the parameter A is given in our case b P 3z /P 1r. The observed scalings for J ma and b ma for two representative runs, along with the epected values of µ J and µ b, are given in Table 1. It can be seen that the results show a ver good agreement with the predictions for the much simpler field configuration. A fan current ma also be obtained in the case of the double null background field. Using the same background field parameters and perturbation as those emploed in the run shown in Figure, the fan localisation shown in Figure (b) is obtained. In this case, the relevant degree of stretching due to the ehaust flow is computed via A = rp 3z /P θ. Observed (plotted in Figure (a)) and epected scalings are given in Table 1, which again demonstrate ver good agreement between the epected values in simple configurations and the behaviour in this more complicated topolog.

13 Spine reconnection For a general disturbance in the fan plane of null, as before, a spine-tpe current sheet results. A tpical localised disturbance is shown in Figure 7(b), and it should be noted that, due to the relativel weak driving flow in the fan close to null, this localisation occurs over man Alfvén times. The single peak (in b) disturbance corresponds to a solitar rotational tube of current centred on the spine. This is the generic current structure for a single disturbance, and a building block for the standard stead-state spine solution of Craig and Fabling (199), in which, due to the smmetries of the coordinate sstem emploed, the spine current sheet is made up of two such tubes. The epected scalings in the dnamic regime of spine current sheets are given b µ J (1 + A)/(A) and µ b 1/(A) (for a field of the form Q, see Heerikhuisen and Craig ). In this case there are two inflow directions and one outflow ( < λ 1 < λ ), and the fastest scaling is obtained when the inflow speeds are equal (λ 1 = λ /, A = 1/), giving clindrical current structures. When λ 1 λ /, the clinder flattens out, and the scaling weakens. We must therefore take A to be the smaller of λ 1 /λ and (λ λ 1 )/λ (for the field Q), or in our case, the smaller of P 3z /P 1r and rp 3z /P θ. A tpical set of results obtained from our simulations is plotted in Figure 7(a). The resultant scaling parameters are again displaed in Table 1. Although the actual values of µ J and µ b are slightl higher than the predicted ones, the basic scaling is of the same order, and still super-fast, in the sense that the reconnection rate ηj will scale as a negative power of η Separator reconnection One might epect that, as in the β > α regime, a suitabl chosen initial disturbance might localise along the separator, to a separator current sheet. This is indeed the case, although one must take care when analsing such a situation. As before, a pulse initiated in the fan of null, but close to the spine of null 1, will localise towards the separator. However, due to the strong driving flow, the localisation and current growth does not halt at this time. Rather, since there is a strong flow along the separator, the disturbance will continue to localise along this direction ( = z = ) and, assuming that the resistivit is sufficientl small, the current will continue to slowl grow until the pulse full localises at null, in a spine current sheet. This effect is shown in Figure, at an intermediate time in the slow localisation along the separator. In the present simulations, we are limited b all of the usual constraints of numerical

14 1 resolution. However, one might epect that if the separator is sufficientl long, or equivalentl if the disturbance is initiated sufficientl close to the separator, that a diffusive current sheet will form at some location on the separator. For this to occur, we require that the time taken for the disturbance to be advected onto the separator (in the perpendicular direction) and form a sheet (τ rec ) be less than the time taken for the flow to push the pulse along the length of the separator (τ sep ) to instead form a current sheet at the null point. In order to obtain some estimate for the length scales involved, we approimate our long separator (in Cartesian coordinates) b the familiar B s = (/l, /l, b ), where l is a magnetic field length scale across the separator, and b is constant. It can then be shown (c.f. Heerikhuisen and Craig ), that if the disturbance has length scale l, then ( α l τ rec l α ln Now, since α > β, the speed of the pulse along the separator is αb. Thus, if the length of the separator is denoted b L, then τ sep L/αb. In our sstem of normalised equations (see Section 3), we have that α, α, b, L 1, and therefore in order that τ rec τ sep we require, if η 1, that l.. This certainl does not seem out with the realms of possibilit in a realistic plasma environment. With η 3, as is tpical in our simulations, we require l.3. This, unfortunatel, is on the boundar of what we can achieve with numerical resolution, so we have been unable to test this idea properl. From the above considerations, it seems unlikel that a long-lived separator current sheet can be formed in this tpe of flu pile-up regime, in which there is alwas a strong flow along the separator itself. In the present eample, the separator current buildup has a miture of fan and spine behaviours, and what is clear is that the nulls themselves pla a crucial role in determining this behaviour. Therefore, in order to obtain a quasi-stead-state current sheet located along (at least the majorit of) the separator, it ma be necessar to consider a compressible collapse-tpe model (e.g. Longcope and Cowle (199), or c.f. Pontin and Craig (5)). η ).. Summar We have investigated the dnamic behaviour of disurbances in the vicinit of a pair of 3D magnetic null points connected b a stable fan-fan separator, in an incompressible, clindrical geometr. It has been shown that the sstem can be analsed in terms of the superposition of transient disturbances onto a background field defining the two-nulls. This result generalizes the previous Cartesian description of transient reconnecting disturbances in a 3D single null geometr (Craig and Fabling 199), as well as stead-state clindrical

15 15 merging solutions (Watson and Craig ; Tassi et al. 3). The behaviour of the sstem falls into two main regimes, depending on the relative magnitudes of the background magnetic field and plasma flow (here β and α, respectivel). If β > α then the background flow is too weak to localize the disturbance field. In this case the magnetic disturbance develops two peaks, and these move in opposite directions along the background field lines. This behaviour is unaffected b changing the sign of either β or α. The pulse that moves inwards towards the null point pair provides the reconnecting field that localises towards either a spine, fan or separator. Of course, a large-scale disturbance, smeared over the entire two-null geometr, ma contain regions which are individuall focussed towards the separator and the nulls. In each case, the localisation is accompanied b a current growth, with the peak current scaling at a slow η. η. with resistivit. This implies that the resulting reconnection is slow, and that the energ release at realistic resistivities is insufficient to account for eplosive phsical processes such as solar flares. This does not, however, preclude these mechanisms from providing background heating in solar or stellar coronae. Rather, our results provide support for magnetic dissipation theories which propose separatrices and separators as preferred sites for background coronal heating (e.g. Priest et al. 5), b demonstrating how transient disturbances are channelled b the background field lines towards such topological features. In order to speed up the reconnection rate, it is necessar to consider the flu pile-up regime associated with strong driving flows α > β. In this regime, both wave solutions for the initial disturbance field travel in the same direction. Initiall, there is a relativel fast equalisation of the magnetic and velocit disturbances to a quasi-stead-state (v (β/α)b). Assuming that the sign of α is chosen to provide inflow, disturbances are localised towards the null separatrices, and ma form spine-aligned current sheets, or fan-aligned current sheets, whose scaling properties with resistivit closel match those at isolated linear nulls in Cartesian geometries. In particular, spine currents scale at a super-fast rate J η 1.5, whereas fan current sheet reconnection models provide more modest current amplitudes of order η.5 η 1, depending on the outflow geometr in the fan. For certain initial parameters and disturbances, a strong separator current ma also result. This current, however, ma not be sustained b the flow geometr. Specificall, the strong driving flow tends to push the pulse towards the spine of the null point whose fan plane corresponds to the inflow direction. Whether the current concentration grows sufficientl strong to begin diffusive/reconnective processes at the separator, or whether this occurs once the disturbance has localised at one of the nulls, depends cruciall on the length scales parallel and perpendicular to the separator. Since the connected null point pair we consider is completel generic as far as the basic field structure is concerned, this behaviour

16 1 ma well be a general propert of two null geometries in strongl driven, incompressible regimes. This interpretation is consistent with the stead-state results of (Watson and Craig ), who found current on the separator onl for ver special choices of boundar conditions. Hence, when modelling energetic phsical processes occuring via reconnection at current sheets along separators, it ma be preferable to consider a compressible collapse-tpe model for the current sheet formation rather than a strongl driven flu pile-up mechanism. Notabl, in the dnamic models described here, the separator localisation contains a hbrid of fan-tpe and spine-tpe behaviours that is strongl affected b the two nulls themselves. The authors would like to acknowledge financial support from the Marsden Fund, grant no. -UOW-5 MIS, and also useful discussions with Paul Watson. A. Appendi The same reduction procedure as described in Section 3 ma be performed for the disturbance form b = a(r, t)ˆθ + b(r, t)ẑ. The resulting differential equations to be solved are a t = (P 1r + κ/l + P 1 r ) [βu αa] + η ( a rr + a r /r a/r ), b t = (P 1 r + κ/l) [βv αb] + η (b rr + b r /r), ( r ) u t = β/r P 1 (ra) r + γl (ra) r /r dr r ( min r ) α/r P 1 (ru) r + γl (ru) r /r dr + ν ( u rr + u r /r u/r ) + g(t), r min v t = (P 1 r κ/l) [βb αv] + ν (v rr + v r /r) + h(t). REFERENCES Albright, B. J. (1999). The densit and clustering of magnetic nulls in stochastic magnetic fields. Phs. Plasmas, :. Antiochos, S. K., Karpen, J. T., and DeVore, C. R. (). Coronal magnetic field relaation b null-point reconnection. Astrophs. J., 575:57 5. Beveridge, C. and Longcope, D. W. (5). On three-dimensional magnetic skeleton elements due to discrete flu sources. Solar Phs., 7:193.

17 17 Run info µ J µ b β > α n loc. A observed epected observed epected 1 F..1 ±..5 1 F.3. ±..5 1 F.5.5 ±.1.5 F..5 ±..5 Sp.51.9 ±..5 Se.5 ±.1.5 α > β 1 F.3. ± ± F..73 ±..73. ± F.7.7 ± ±..35 F..7 ±..7.1 ±.. Sp ± ±..93 Table 1: Scaling results from the simulations and predictions based on previous analtical work. Column 1 (n) gives the number of nulls in the field for that run, column denotes which topological feature the current localises towards (F=fan, Sp=spine, Se=separator), and A is the isotrop of the corresponding null. Observed results are calculated b linear regression, with errors given at 95% confidence level.

18 1 Craig, I. J. D. and Fabling, R. B. (199). Eact solutions for stead-state, spine, and fan magnetic reconnection. Astrophs. J., : Craig, I. J. D. and Fabling, R. B. (199). Dnamic magnetic reconnection in three space dimensions: Fan current solutions. Phs. Plasmas, 5:35. Craig, I. J. D., Fabling, R. B., Heerikhuisen, J., and Watson, P. G. (1999). Magnetic reconnection solutions in the presence of multiple nulls. Astrophs. J., 53:3. Craig, I. J. D., Fabling, R. B., Henton, S. M., and Rickard, G. J. (1995). An eact solution for stead state magnetic reconnection in three dimensions. Astrophs. J. Lett., 55:L197 L199. Craig, I. J. D. and Henton, S. M. (1995). Eact solutions for stead state incompressible magnetic reconnection. Astrophs. J., 5:. Craig, I. J. D. and Watson, P. G. (3). Magnetic reconnection solutions based on a generalised ohm s law. Solar Phs., 1: Craig, I. J. D. and Watson, P. G. (5). Eact models for Hall current reconnection with aial guide fields. Phs. Plasmas, 1:13. Fletcher, L., Metcalf, T. R., Aleander, D., Brown, D. S., and Rder, L. A. (1). Evidence for the flare trigger site and three-dimensional reconnection in multiwavelength observations of a solar flare. Astrophs. J., 55:51 3. Fukao, S., Ugai, M., and Tsuda, T. (1975). Topological stud of magnetic field near a neutral point. Rep. Ion. Sp. Res. Japan, 9: Heerikhuisen, J. and Craig, I. J. D. (). Magnetic reconnection in three dimensions - spine, fan and separator solutions. Solar Phs., : Inverarit, G. W. and Priest, E. R. (1999). Magnetic null points due to multiple sources of solar photospheric flu. Solar Phs., 1: Ji, H. S. and Song, M. T. (1). Three-dimensional solutions for fan and spine magnetic reconnection in partiall ionized plasmas. Astrophs. J., 55:17. Lau, Y. T. and Finn, J. M. (199). Three dimensional kinematic reconnection in the presence of field nulls and closed field lines. Astrophs. J., 35:7 91. Litvinenko, Y. E. and Craig, I. J. D. Robust scalings in compressible flu pile-up reconnection. Solar Phs., 1:

19 19 Longcope, D. W. (199). Topolog and current ribbons: A model for current, reconnection and flaring in a comple, evolving corona. Solar Phs., 19: Longcope, D. W., Brown, D. S., and Priest, E. R. (3). On the distribution of magnetic null points above the solar photosphere. Phs. Plasmas, : Longcope, D. W. and Cowle, S. C. (199). Current sheet formation along three-dimensional magnetic separators. Phs. Plasmas, 3:5 97. Longcope, D. W., Kankelborg, C. C., Nelson, J. L., and Petsov, A. A. (1). Evidence of separator reconnection in a surve of -ra bright points. Astrophs. J., 553:9 39. Longcope, D. W., McKenzie, D., Cirtain, J., and Scott, J. (5). Observations of separator reconnection to an emerging active region. Astrophs. J., 3:59. Longcope, D. W. and Noonan, E. J. (). Self-organised criticalit from separator reconnection in solar flares. Astrophs. J., 5: 99. Parnell, C. E. and Galsgaard, K. (). Elementar heating events - magnetic interactions between two flu sources. ii rates of flu reconnection. Astron. Astrophs., : Parnell, C. E., Smith, J. M., Neukirch, T., and Priest, E. R. (199). The structure of three-dimensional magnetic neutral points. Phs. Plasmas, 3(3): Pontin, D. I. and Craig, I. J. D. (5). Current singularities at finitel compressible threedimensional magnetic null points. Phs. Plasmas, 1:711. Priest, E. R., Longcope, D. W., and Hevaerts, J. F. (5). Coronal heating at separators and separatrices. Astrophs. J., : Priest, E. R. and Titov, V. S. (199). Magnetic reconnection at three-dimensional null points. Phil. Trans. R. Soc. Lond. A, 35: Schrijver, C. J. and Title, A. M. (). The topolog of a mied-polarit potential field, and inferences for the heating of the quiet solar corona. Solar Phs., 7:3. Tassi, E., Titov, V. S., and Hornig, G. (3). Eact solutions for reconnective annihilation in magnetic configurations with three sources. Phs. Plasmas, :. Watson, P. G. and Craig, I. J. D. (). Analtic magnetic reconnection solutions in clindrical geometr. Solar Phs., 7:

20 Wheatland, M. S. (). Distribution of flare energies based on independent reconnecting structures. Solar Phs., :33. This preprint was prepared with the AAS L A TEX macros v5..

21 1 (a) (b) Fig. 1. Field lines of the skeleton of the background field P, when (a) κ and γ are of the same sign and a single null is present, and (b) κ and γ are opposite signs and γ > κ e, giving two nulls (with κ > in each case). The gre lines indicate the shape of the domain and the locations of the fan planes of the nulls.

22 Fig.. Evolution of a magnetic field disturbance (black red online) in rθ, with the ingoing peak forming a current in the fan plane of null 1. The dots indicate the positions of the nulls, and the dotted line is the separator, while the gre lines (white online) show some planar-projected representative field lines of P. The shading in each image, taken at times t =, 3.,.3, 11., is scaled to the maimum in that frame, and the chosen parameters are α =., β = 1, γ = 1, κ =.33 and l = 5.

23 Fig. 3. As Fig.. The ingoing peak forms a current moving towards the spine of null. The shading in each image, taken at times t =, 7.7, 1., 1.7, is scaled to the maimum in that frame, and the chosen parameters are α =., β = 1, γ = 1, κ =.5 and l = 3.

24 Fig.. As Fig.. The ingoing peak forms a current in the vicinit of the separator. The shading in each image, taken at times t =,., 11., 19.3, is scaled to the maimum in that frame, and the chosen parameters are α =., β = 1, γ = 1, κ =.3 and l = 5.

25 5.5.5 ln ( J ma ) ln (η) Fig. 5. Scaling of the peak current with resistivit and best-fit lines to the data, in the regime β > α, for the single null with curved fan current buildup (stars), and the double null fan current (diamonds), spine current (squares), and separator current (circles) runs Fan localisation ln(j );(i) ma ln(b ma );(i) ln(j ma );(ii) ln(b ma );(ii) b ln (η) Fig.. (a) Scaling of the peak current (J ma ) and maimum field at time of peak current (b ma ) with resistivit, and best fit lines, for fan currents in the presence of one null (run (i); µ J =.73, µ b =.) and two nulls (run (ii); µ J =.7, µ b =.1). (b) Tpical disturbance field profile at time of J ma for the two null field, for parameters α =, β =., γ = 1, κ =.33, l = 5.

26 Spine localisation 7 ln(j ma ) ln(b ma ) 5 3 b ln (η) Fig. 7. (a) Scaling of the peak current (J ma ) and maimum field at time of peak current (b ma ) with resistivit, and best fit lines, for the spine current, giving µ J = 1.9, µ b =.91. (b) Tpical disturbance field profile at time of J ma. Parameters are α =, β =, γ = 1, κ =.5, l = 3.

27 7 b Fig.. Tpical disturbance field profile for a separator current, during the slow localisation phase along separator, for parameters α =, β =., γ = 1, κ =.3, l = 5. Plotted on top of the bo are the positions of the null points and separator.

KINEMATIC MAGNETIC RECONNECTION AT 3D NULL POINTS

KINEMATIC MAGNETIC RECONNECTION AT 3D NULL POINTS KINEMATIC MAGNETIC RECONNECTION AT 3D NULL POINTS D. I. Pontin, G. Hornig, and E. R. Priest Mathematical Institute, Universit of St Andrews, St Andrews, Fife, KY6 9SS, UK, Email: davidp@mcs.st-and.ac.uk

More information

Magnetic reconnection in coronal plasmas

Magnetic reconnection in coronal plasmas UW, 28 May, 2010 p.1/17 Magnetic reconnection in coronal plasmas I.J.D Craig Department of Mathematics University of Waikato Hamilton New Zealand UW, 28 May, 2010 p.2/17 Why reconnection? Reconnection

More information

KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT: SPINE-ALIGNED CURRENT

KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT: SPINE-ALIGNED CURRENT Geophsical and Astrophsical Fluid Dnamics Vol. 98, No. 5, October, pp. 7 8 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT: SPINE-ALIGNED CURRENT D.I. PONTIN a, *, G. HORNIG b and E.R. PRIEST a a School

More information

Fast magnetic reconnection via jets and current micro-sheets

Fast magnetic reconnection via jets and current micro-sheets Fast magnetic reconnection via jets and current micro-sheets P. G. Watson Center for Magnetic Reconnection Studies, Institute for Fusion Studies, Department of Physics, University of Texas at Austin, Austin,

More information

Current sheet formation and non-ideal behaviour at three-dimensional magnetic null points. Abstract

Current sheet formation and non-ideal behaviour at three-dimensional magnetic null points. Abstract APS/123-QED Current sheet formation and non-ideal behaviour at three-dimensional magnetic null points D. I. Pontin and A. Bhattacharjee Space Science Center, University of New Hampshire, Durham, New Hampshire,

More information

Exact solutions for magnetic annihilation in curvilinear geometry

Exact solutions for magnetic annihilation in curvilinear geometry Exact solutions for magnetic annihilation in curvilinear geometry E. Tassi b,, V.S. Titov and G. Hornig Theoretische Physik IV, Ruhr-Universität Bochum, 44780 Bochum, Germany b Theoretische Physik IV,

More information

Spine-Fan reconnection

Spine-Fan reconnection Astronom & Astrophsics manuscript no. WperJain3 c ESO 202 August, 202 Spine-Fan reconnection The influence of temporal and spatial variation in the driver P. F. Wper, Rekha Jain, and D. I. Pontin 2 School

More information

Magnetic Reconnection: Recent Developments and Future Challenges

Magnetic Reconnection: Recent Developments and Future Challenges Magnetic Reconnection: Recent Developments and Future Challenges A. Bhattacharjee Center for Integrated Computation and Analysis of Reconnection and Turbulence (CICART) Space Science Center, University

More information

CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL

CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL Mathematical and Computational Applications,Vol. 15, No. 4, pp. 742-761, 21. c Association for Scientific Research CONSERVATION LAWS AND CONSERVED QUANTITIES FOR LAMINAR RADIAL JETS WITH SWIRL R. Naz 1,

More information

Reduced MHD. Nick Murphy. Harvard-Smithsonian Center for Astrophysics. Astronomy 253: Plasma Astrophysics. February 19, 2014

Reduced MHD. Nick Murphy. Harvard-Smithsonian Center for Astrophysics. Astronomy 253: Plasma Astrophysics. February 19, 2014 Reduced MHD Nick Murphy Harvard-Smithsonian Center for Astrophysics Astronomy 253: Plasma Astrophysics February 19, 2014 These lecture notes are largely based on Lectures in Magnetohydrodynamics by Dalton

More information

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin.

THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin. THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY 1. Introduction V. A. Sharifulin Perm State Technical Universit, Perm, Russia e-mail: sharifulin@perm.ru Water

More information

Finite-time singularity formation at a magnetic neutral line in Hall magnetohydrodynamics

Finite-time singularity formation at a magnetic neutral line in Hall magnetohydrodynamics Finite-time singularity formation at a magnetic neutral line in Hall magnetohydrodynamics Yuri E. Litvinenko, Liam C. McMahon Department of Mathematics, University of Waikato, P. B. 3105, Hamilton, New

More information

x y plane is the plane in which the stresses act, yy xy xy Figure 3.5.1: non-zero stress components acting in the x y plane

x y plane is the plane in which the stresses act, yy xy xy Figure 3.5.1: non-zero stress components acting in the x y plane 3.5 Plane Stress This section is concerned with a special two-dimensional state of stress called plane stress. It is important for two reasons: () it arises in real components (particularl in thin components

More information

1.1 The Equations of Motion

1.1 The Equations of Motion 1.1 The Equations of Motion In Book I, balance of forces and moments acting on an component was enforced in order to ensure that the component was in equilibrium. Here, allowance is made for stresses which

More information

EP225 Note No. 4 Wave Motion

EP225 Note No. 4 Wave Motion EP5 Note No. 4 Wave Motion 4. Sinusoidal Waves, Wave Number Waves propagate in space in contrast to oscillations which are con ned in limited regions. In describing wave motion, spatial coordinates enter

More information

Two-Dimensional Analysis of the Power Transfer between Crossed Laser Beams

Two-Dimensional Analysis of the Power Transfer between Crossed Laser Beams Two-Dimensional Analsis of the Power Transfer between Crossed Laser Beams The indirect-drive approach to inertial confinement fusion involves laser beams that cross as the enter the hohlraum. Ionacoustic

More information

Simulation of Electric Fields in Small Size Divertor Tokamak Plasma Edge

Simulation of Electric Fields in Small Size Divertor Tokamak Plasma Edge Energ and Power Engineering, 21, 39-45 doi:1.4236/epe.21.217 Published Online Februar 21 (http://www.scirp.org/journal/epe) Simulation of Electric Fields in Small Size Divertor Tokamak Plasma Edge Plasma

More information

Scaling of asymmetric magnetic reconnection: Kinetic particle in cell simulations

Scaling of asymmetric magnetic reconnection: Kinetic particle in cell simulations JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 115,, doi:10.109/010ja01545, 010 Scaling of asmmetric magnetic reconnection: Kinetic particle in cell simulations K. Malakit, 1 M. A. Sha, 1 P. A. Cassak, and C. Bard

More information

UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX METHOD

UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX METHOD Proceedings of the 3rd ASME/JSME Joint Fluids Engineering Conference Jul 8-23, 999, San Francisco, California FEDSM99-8 UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX

More information

The first change comes in how we associate operators with classical observables. In one dimension, we had. p p ˆ

The first change comes in how we associate operators with classical observables. In one dimension, we had. p p ˆ VI. Angular momentum Up to this point, we have been dealing primaril with one dimensional sstems. In practice, of course, most of the sstems we deal with live in three dimensions and 1D quantum mechanics

More information

Consideration of Shock Waves in Airbag Deployment Simulations

Consideration of Shock Waves in Airbag Deployment Simulations Consideration of Shock Waves in Airbag Deploment Simulations Doris Rieger BMW Group ABSTRACT When the inflation process of a simple flat airbag was simulated with the MADYMO gas flow module, the resulting

More information

Joule Heating Effects on MHD Natural Convection Flows in Presence of Pressure Stress Work and Viscous Dissipation from a Horizontal Circular Cylinder

Joule Heating Effects on MHD Natural Convection Flows in Presence of Pressure Stress Work and Viscous Dissipation from a Horizontal Circular Cylinder Journal of Applied Fluid Mechanics, Vol. 7, No., pp. 7-3, 04. Available online at www.jafmonline.net, ISSN 735-357, EISSN 735-3645. Joule Heating Effects on MHD Natural Convection Flows in Presence of

More information

Mechanics Departmental Exam Last updated November 2013

Mechanics Departmental Exam Last updated November 2013 Mechanics Departmental Eam Last updated November 213 1. Two satellites are moving about each other in circular orbits under the influence of their mutual gravitational attractions. The satellites have

More information

Anisotropic viscous dissipation in compressible magnetic X-points

Anisotropic viscous dissipation in compressible magnetic X-points Astronomy & Astrophysics manuscript no. icvis8 c ESO 28 June 8, 28 Anisotropic viscous dissipation in compressible magnetic X-points I. J. D. Craig Department of Mathematics, University of Waikato, P.

More information

MAE 323: Chapter 4. Plane Stress and Plane Strain. The Stress Equilibrium Equation

MAE 323: Chapter 4. Plane Stress and Plane Strain. The Stress Equilibrium Equation The Stress Equilibrium Equation As we mentioned in Chapter 2, using the Galerkin formulation and a choice of shape functions, we can derive a discretized form of most differential equations. In Structural

More information

NONLINEAR DYNAMICS AND CHAOS. Numerical integration. Stability analysis

NONLINEAR DYNAMICS AND CHAOS. Numerical integration. Stability analysis LECTURE 3: FLOWS NONLINEAR DYNAMICS AND CHAOS Patrick E McSharr Sstems Analsis, Modelling & Prediction Group www.eng.o.ac.uk/samp patrick@mcsharr.net Tel: +44 83 74 Numerical integration Stabilit analsis

More information

Physics Gravitational force. 2. Strong or color force. 3. Electroweak force

Physics Gravitational force. 2. Strong or color force. 3. Electroweak force Phsics 360 Notes on Griffths - pluses and minuses No tetbook is perfect, and Griffithsisnoeception. Themajorplusisthat it is prett readable. For minuses, see below. Much of what G sas about the del operator

More information

SMALL bodies of the solar system, such as Phobos, cannot

SMALL bodies of the solar system, such as Phobos, cannot INSTITUTO SUPERIOR TÉCNICO, LISBON, PORTUGAL, JUNE 013 1 Controlled Approach Strategies on Small Celestial Bodies Using Approimate Analtical Solutions of the Elliptical Three-Bod Problem: Application to

More information

UNIT 4 HEAT TRANSFER BY CONVECTION

UNIT 4 HEAT TRANSFER BY CONVECTION UNIT 4 HEAT TRANSFER BY CONVECTION 4.1 Introduction to convection 4. Convection boundar laers 4..1 Hdrodnamic boundar laer over flat plate 4.. Thermal boundar laer 4..3 Concentration boundar laer 4.3 Dimensional

More information

Velocity Limit in DPD Simulations of Wall-Bounded Flows

Velocity Limit in DPD Simulations of Wall-Bounded Flows Velocit Limit in DPD Simulations of Wall-Bounded Flows Dmitr A. Fedosov, Igor V. Pivkin and George Em Karniadakis Division of Applied Mathematics, Brown Universit, Providence, RI 2912 USA Abstract Dissipative

More information

Exercise solutions: concepts from chapter 5

Exercise solutions: concepts from chapter 5 1) Stud the oöids depicted in Figure 1a and 1b. a) Assume that the thin sections of Figure 1 lie in a principal plane of the deformation. Measure and record the lengths and orientations of the principal

More information

4 Strain true strain engineering strain plane strain strain transformation formulae

4 Strain true strain engineering strain plane strain strain transformation formulae 4 Strain The concept of strain is introduced in this Chapter. The approimation to the true strain of the engineering strain is discussed. The practical case of two dimensional plane strain is discussed,

More information

Research Article Development of a Particle Interaction Kernel Function in MPS Method for Simulating Incompressible Free Surface Flow

Research Article Development of a Particle Interaction Kernel Function in MPS Method for Simulating Incompressible Free Surface Flow Journal of Applied Mathematics Volume 2, Article ID 793653, 6 pages doi:.55/2/793653 Research Article Development of a Particle Interaction Kernel Function in MPS Method for Simulating Incompressible Free

More information

Why are flare ribbons associated with the spines of magnetic null points generically elongated?

Why are flare ribbons associated with the spines of magnetic null points generically elongated? Solar Physics DOI: 10.1007/ - - - - Why are flare ribbons associated with the spines of magnetic null points generically elongated? David Pontin 1 Klaus Galsgaard 2 Pascal Démoulin 3 c Springer Abstract

More information

MAGNETIC NOZZLE PLASMA EXHAUST SIMULATION FOR THE VASIMR ADVANCED PROPULSION CONCEPT

MAGNETIC NOZZLE PLASMA EXHAUST SIMULATION FOR THE VASIMR ADVANCED PROPULSION CONCEPT MAGNETIC NOZZLE PLASMA EXHAUST SIMULATION FOR THE VASIMR ADVANCED PROPULSION CONCEPT ABSTRACT A. G. Tarditi and J. V. Shebalin Advanced Space Propulsion Laboratory NASA Johnson Space Center Houston, TX

More information

MAGNETOHYDRODYNAMICS - 2 (Sheffield, Sept 2003) Eric Priest. St Andrews

MAGNETOHYDRODYNAMICS - 2 (Sheffield, Sept 2003) Eric Priest. St Andrews MAGNETOHYDRODYNAMICS - 2 (Sheffield, Sept 2003) Eric Priest St Andrews CONTENTS - Lecture 2 1. Introduction 2. Flux Tubes *Examples 3. Fundamental Equations 4. Induction Equation *Examples 5. Equation

More information

Phase mixing of shear Alfvén waves as a new mechanism for electron acceleration in collisionless, kinetic plasmas

Phase mixing of shear Alfvén waves as a new mechanism for electron acceleration in collisionless, kinetic plasmas Phase mixing of shear Alfvén waves as a new mechanism for electron acceleration in collisionless, kinetic plasmas Tsiklauri, D, Sakai, J I and Saito, S http://dx.doi.org/10.1088/1367 2630/7/1/079 Title

More information

Solar coronal heating by magnetic cancellation: I. connected equal bipoles

Solar coronal heating by magnetic cancellation: I. connected equal bipoles Mon. Not. R. Astron. Soc., () Printed 5 August 25 (MN LATEX style file v2.2) Solar coronal heating by magnetic cancellation: I. connected equal bipoles B. von Rekowski, C. E. Parnell and E. R. Priest School

More information

5.3.3 The general solution for plane waves incident on a layered halfspace. The general solution to the Helmholz equation in rectangular coordinates

5.3.3 The general solution for plane waves incident on a layered halfspace. The general solution to the Helmholz equation in rectangular coordinates 5.3.3 The general solution for plane waves incident on a laered halfspace The general solution to the elmhol equation in rectangular coordinates The vector propagation constant Vector relationships between

More information

An elementary model for the validation of flamelet approximations in non-premixed turbulent combustion

An elementary model for the validation of flamelet approximations in non-premixed turbulent combustion Combust. Theor Modelling 4 () 89. Printed in the UK PII: S364-783()975- An elementar model for the validation of flamelet approimations in non-premied turbulent combustion A Bourliou and A J Majda Département

More information

Strain Transformation and Rosette Gage Theory

Strain Transformation and Rosette Gage Theory Strain Transformation and Rosette Gage Theor It is often desired to measure the full state of strain on the surface of a part, that is to measure not onl the two etensional strains, and, but also the shear

More information

Functions of Several Variables

Functions of Several Variables Chapter 1 Functions of Several Variables 1.1 Introduction A real valued function of n variables is a function f : R, where the domain is a subset of R n. So: for each ( 1,,..., n ) in, the value of f is

More information

Module 1 : The equation of continuity. Lecture 4: Fourier s Law of Heat Conduction

Module 1 : The equation of continuity. Lecture 4: Fourier s Law of Heat Conduction 1 Module 1 : The equation of continuit Lecture 4: Fourier s Law of Heat Conduction NPTEL, IIT Kharagpur, Prof. Saikat Chakrabort, Department of Chemical Engineering Fourier s Law of Heat Conduction According

More information

520 Chapter 9. Nonlinear Differential Equations and Stability. dt =

520 Chapter 9. Nonlinear Differential Equations and Stability. dt = 5 Chapter 9. Nonlinear Differential Equations and Stabilit dt L dθ. g cos θ cos α Wh was the negative square root chosen in the last equation? (b) If T is the natural period of oscillation, derive the

More information

Chapter 3. Theory of measurement

Chapter 3. Theory of measurement Chapter. Introduction An energetic He + -ion beam is incident on thermal sodium atoms. Figure. shows the configuration in which the interaction one is determined b the crossing of the laser-, sodium- and

More information

MHD Simulation of Solar Chromospheric Evaporation Jets in the Oblique Coronal Magnetic Field

MHD Simulation of Solar Chromospheric Evaporation Jets in the Oblique Coronal Magnetic Field MHD Simulation of Solar Chromospheric Evaporation Jets in the Oblique Coronal Magnetic Field Y. Matsui, T. Yokoyama, H. Hotta and T. Saito Department of Earth and Planetary Science, University of Tokyo,

More information

BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS

BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS Koung-Heog LEE 1, Subhash C GOEL 2 And Bozidar STOJADINOVIC 3 SUMMARY Full restrained beam-to-column connections in steel moment resisting frames have been

More information

THE IMPACT OF MICROSCOPIC MAGNETIC RECONNECTION ON PRE-FLARE ENERGY STORAGE

THE IMPACT OF MICROSCOPIC MAGNETIC RECONNECTION ON PRE-FLARE ENERGY STORAGE The Astrophsical Journal, 77:L158 L16, 9 December C 9. The American Astronomical Societ. All rights reserved. Printed in the U.S.A. doi:1.188/4-637x/77//l158 THE IMPACT OF MICROSCOPIC MAGNETIC RECONNECTION

More information

Control of quantum two-level systems

Control of quantum two-level systems Control of quantum two-level sstems R. Gross, A. Mar & F. Deppe, Walther-Meißner-Institut (00-03) 0.3 Control of quantum two-level sstems.. General concept AS-Chap. 0 - How to control a qubit? Does the

More information

x find all of the symmetry operations/elements: o character table headings: E, 2C φ σ v, i, S φ C 2 φ

x find all of the symmetry operations/elements: o character table headings: E, 2C φ σ v, i, S φ C 2 φ Construct and annotate a valence molecular orbital diagram for the linear molecule Mg 2. Assume the 3pAOs lie deeper in energ than the Mg 3sAO and that the Mg and orbitals interact onl slightl. Mg is a

More information

The Gas-assisted Expelled Fluid Flow in the Front of a Long Bubble in a Channel

The Gas-assisted Expelled Fluid Flow in the Front of a Long Bubble in a Channel C. H. Hsu, P. C. Chen,. Y. ung, G. C. uo The Gas-assisted Epelled Fluid Flow in the Front of a Long Bubble in a Channel C.H. Hsu 1, P.C. Chen 3,.Y. ung, and G.C. uo 1 1 Department of Mechanical Engineering

More information

10 Back to planar nonlinear systems

10 Back to planar nonlinear systems 10 Back to planar nonlinear sstems 10.1 Near the equilibria Recall that I started talking about the Lotka Volterra model as a motivation to stud sstems of two first order autonomous equations of the form

More information

RECURSIVE RECONNECTION AND MAGNETIC SKELETONS

RECURSIVE RECONNECTION AND MAGNETIC SKELETONS The Astrophysical Journal, 675:1656 1665, 2008 March 10 # 2008. The American Astronomical Society. All rights reserved. Printed in U.S.A. A RECURSIVE RECONNECTION AND MAGNETIC SKELETONS C. E. Parnell and

More information

A HAND-HELD SENSOR FOR LOCAL MEASUREMENT OF MAGNETIC FIELD, INDUCTION AND ENERGY LOSSES

A HAND-HELD SENSOR FOR LOCAL MEASUREMENT OF MAGNETIC FIELD, INDUCTION AND ENERGY LOSSES A HAND-HELD SENSOR FOR LOCAL MEASUREMENT OF MAGNETIC FIELD, INDUCTION AND ENERGY LOSSES G. Krismanic, N. Baumgartinger and H. Pfützner Institute of Fundamentals and Theor of Electrical Engineering Bioelectricit

More information

Solar coronal heating by magnetic cancellation: II. disconnected and unequal bipoles

Solar coronal heating by magnetic cancellation: II. disconnected and unequal bipoles Mon. Not. R. Astron. Soc., () Printed 14 December 25 (MN LATEX style file v2.2) Solar coronal heating by magnetic cancellation: II. disconnected and unequal bipoles B. von Rekowski, C. E. Parnell and E.

More information

CONTINUOUS SPATIAL DATA ANALYSIS

CONTINUOUS SPATIAL DATA ANALYSIS CONTINUOUS SPATIAL DATA ANALSIS 1. Overview of Spatial Stochastic Processes The ke difference between continuous spatial data and point patterns is that there is now assumed to be a meaningful value, s

More information

EVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING

EVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING EVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING A Thesis b BRENT DURRELL PICKLE Submitted to the Office of Graduate Studies of Teas A&M Universit in partial fulfillment

More information

Dynamics of multiple pendula without gravity

Dynamics of multiple pendula without gravity Chaotic Modeling and Simulation (CMSIM) 1: 57 67, 014 Dnamics of multiple pendula without gravit Wojciech Szumiński Institute of Phsics, Universit of Zielona Góra, Poland (E-mail: uz88szuminski@gmail.com)

More information

ME615 Project Report Aeroacoustic Simulations using Lattice Boltzmann Method

ME615 Project Report Aeroacoustic Simulations using Lattice Boltzmann Method ME615 Project Report Aeroacoustic Simulations using Lattice Boltzmann Method Kameswararao Anupindi School of Mechanical Engineering, Purdue Universit, West Lafaette, IN, 4796, USA Lattice Boltzmann method

More information

Coronal Magnetic Field Extrapolations

Coronal Magnetic Field Extrapolations 3 rd SOLAIRE School Solar Observational Data Analysis (SODAS) Coronal Magnetic Field Extrapolations Stéphane RÉGNIER University of St Andrews What I will focus on Magnetic field extrapolation of active

More information

Physical modeling of coronal magnetic fields and currents

Physical modeling of coronal magnetic fields and currents Physical modeling of coronal magnetic fields and currents Participants: E. Elkina,, B. Nikutowski,, A. Otto, J. Santos (Moscow,Lindau,, Fairbanks, São José dos Campos) Goal: Forward modeling to understand

More information

International Journal of Scientific Research and Reviews

International Journal of Scientific Research and Reviews Research article Available online www.ijsrr.org ISSN: 2279 543 International Journal of Scientific Research and Reviews Soret effect on Magneto Hdro Dnamic convective immiscible Fluid flow in a Horizontal

More information

Mathematics 309 Conic sections and their applicationsn. Chapter 2. Quadric figures. ai,j x i x j + b i x i + c =0. 1. Coordinate changes

Mathematics 309 Conic sections and their applicationsn. Chapter 2. Quadric figures. ai,j x i x j + b i x i + c =0. 1. Coordinate changes Mathematics 309 Conic sections and their applicationsn Chapter 2. Quadric figures In this chapter want to outline quickl how to decide what figure associated in 2D and 3D to quadratic equations look like.

More information

Fast waves during transient flow in an asymmetric channel

Fast waves during transient flow in an asymmetric channel Int. Conference on Boundar and Interior Laers BAIL 6 G. Lube, G. Rapin (Eds) c Universit of Göttingen, German, 6. Introduction Fast waves during transient flow in an asmmetric channel Dick Kachuma & Ian

More information

CHAPTER 2: Partial Derivatives. 2.2 Increments and Differential

CHAPTER 2: Partial Derivatives. 2.2 Increments and Differential CHAPTER : Partial Derivatives.1 Definition of a Partial Derivative. Increments and Differential.3 Chain Rules.4 Local Etrema.5 Absolute Etrema 1 Chapter : Partial Derivatives.1 Definition of a Partial

More information

Symmetry Arguments and the Role They Play in Using Gauss Law

Symmetry Arguments and the Role They Play in Using Gauss Law Smmetr Arguments and the Role The la in Using Gauss Law K. M. Westerberg (9/2005) Smmetr plas a ver important role in science in general, and phsics in particular. Arguments based on smmetr can often simplif

More information

MHD wave propagation in the neighbourhood of a two-dimensional null point. J. A. McLaughlin and A. W. Hood

MHD wave propagation in the neighbourhood of a two-dimensional null point. J. A. McLaughlin and A. W. Hood A&A 420, 1129 1140 (2004) DOI: 10.1051/0004-6361:20035900 c ESO 2004 Astronomy & Astrophysics MHD wave propagation in the neighbourhood of a two-dimensional null point J. A. McLaughlin and A. W. Hood School

More information

Plasma spectroscopy when there is magnetic reconnection associated with Rayleigh-Taylor instability in the Caltech spheromak jet experiment

Plasma spectroscopy when there is magnetic reconnection associated with Rayleigh-Taylor instability in the Caltech spheromak jet experiment Plasma spectroscopy when there is magnetic reconnection associated with Rayleigh-Taylor instability in the Caltech spheromak jet experiment KB Chai Korea Atomic Energy Research Institute/Caltech Paul M.

More information

Numerical experiments on wave propagation toward a 3D null point due to rotational motions

Numerical experiments on wave propagation toward a 3D null point due to rotational motions JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 108, NO. A1, 1042, doi:10.1029/2002ja009393, 2003 Numerical experiments on wave propagation toward a 3D null point due to rotational motions K. Galsgaard and E. R.

More information

Consider a slender rod, fixed at one end and stretched, as illustrated in Fig ; the original position of the rod is shown dotted.

Consider a slender rod, fixed at one end and stretched, as illustrated in Fig ; the original position of the rod is shown dotted. 4.1 Strain If an object is placed on a table and then the table is moved, each material particle moves in space. The particles undergo a displacement. The particles have moved in space as a rigid bod.

More information

Origin of Anomalous Resistivity in Collisionless Reconnection

Origin of Anomalous Resistivity in Collisionless Reconnection APFA & APPTC, Oct.267-30, 2009, Aomori, Japan Origin of Anomalous Resistivit in Collisionless Reconnection Ritoku Horiuchi 1) Toseo Moritaka 2) 1) National Institute for Fusion Science and the Graduate

More information

NANOFLARES HEATING OF SOLAR CORONA BY RECONNECTION MODEL

NANOFLARES HEATING OF SOLAR CORONA BY RECONNECTION MODEL NANOFLARES HEATING OF SOLAR CORONA BY RECONNECTION MODEL VINOD KUMAR JOSHI 1, LALAN PRASAD 2 1 Department of Electronics and Communication, Manipal Institute of Technology, Manipal-576104, India E-mail:

More information

C. Non-linear Difference and Differential Equations: Linearization and Phase Diagram Technique

C. Non-linear Difference and Differential Equations: Linearization and Phase Diagram Technique C. Non-linear Difference and Differential Equations: Linearization and Phase Diaram Technique So far we have discussed methods of solvin linear difference and differential equations. Let us now discuss

More information

Solar Flare. A solar flare is a sudden brightening of solar atmosphere (photosphere, chromosphere and corona)

Solar Flare. A solar flare is a sudden brightening of solar atmosphere (photosphere, chromosphere and corona) Solar Flares Solar Flare A solar flare is a sudden brightening of solar atmosphere (photosphere, chromosphere and corona) Flares release 1027-1032 ergs energy in tens of minutes. (Note: one H-bomb: 10

More information

The Basic (Physical) Problem: Experiments. Internal Gravity Waves and Hyperbolic Boundary-Value Problems. Internal Gravity Waves. Governing Equations

The Basic (Physical) Problem: Experiments. Internal Gravity Waves and Hyperbolic Boundary-Value Problems. Internal Gravity Waves. Governing Equations The Basic (Phsical) Problem: Eperiments Internal Gravit Waves and Hperbolic Boundar-Value Problems P. A. Martin Colorado chool of Mines Collaborator: tefan Llewelln mith, UC an Diego D. E. Mowbra & B..

More information

c 1999 Society for Industrial and Applied Mathematics

c 1999 Society for Industrial and Applied Mathematics SIAM J. SCI. COMPUT. Vol., No. 6, pp. 978 994 c 999 Societ for Industrial and Applied Mathematics A STUDY OF MONITOR FUNCTIONS FOR TWO-DIMENSIONAL ADAPTIVE MESH GENERATION WEIMING CAO, WEIZHANG HUANG,

More information

Elliptic Equations. Chapter Definitions. Contents. 4.2 Properties of Laplace s and Poisson s Equations

Elliptic Equations. Chapter Definitions. Contents. 4.2 Properties of Laplace s and Poisson s Equations 5 4. Properties of Laplace s and Poisson s Equations Chapter 4 Elliptic Equations Contents. Neumann conditions the normal derivative, / = n u is prescribed on the boundar second BP. In this case we have

More information

arxiv: v2 [nlin.cd] 24 Aug 2018

arxiv: v2 [nlin.cd] 24 Aug 2018 3D billiards: visualization of regular structures and trapping of chaotic trajectories arxiv:1805.06823v2 [nlin.cd] 24 Aug 2018 Markus Firmbach, 1, 2 Steffen Lange, 1 Roland Ketzmerick, 1, 2 and Arnd Bäcker

More information

AE/ME 339. K. M. Isaac Professor of Aerospace Engineering. December 21, 2001 topic13_grid_generation 1

AE/ME 339. K. M. Isaac Professor of Aerospace Engineering. December 21, 2001 topic13_grid_generation 1 AE/ME 339 Professor of Aerospace Engineering December 21, 2001 topic13_grid_generation 1 The basic idea behind grid generation is the creation of the transformation laws between the phsical space and the

More information

Multi-body modeling for fluid sloshing dynamics investigation in fast spinning rockets

Multi-body modeling for fluid sloshing dynamics investigation in fast spinning rockets DOI:.9/EUCASS7-47 7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) Multi-bod modeling for fluid sloshing dnamics investigation in fast spinning rockets Loreno Bucci, Michèle Lavagna

More information

Optimal scaling of the random walk Metropolis on elliptically symmetric unimodal targets

Optimal scaling of the random walk Metropolis on elliptically symmetric unimodal targets Optimal scaling of the random walk Metropolis on ellipticall smmetric unimodal targets Chris Sherlock 1 and Gareth Roberts 2 1. Department of Mathematics and Statistics, Lancaster Universit, Lancaster,

More information

Methods of Solving Ordinary Differential Equations (Online)

Methods of Solving Ordinary Differential Equations (Online) 7in 0in Felder c0_online.te V3 - Januar, 05 0:5 A.M. Page CHAPTER 0 Methods of Solving Ordinar Differential Equations (Online) 0.3 Phase Portraits Just as a slope field (Section.4) gives us a wa to visualize

More information

Pan Pearl River Delta Physics Olympiad 2005

Pan Pearl River Delta Physics Olympiad 2005 1 Jan. 29, 25 Morning Session (9 am 12 pm) Q1 (5 Two identical worms of length L are ling on a smooth and horizontal surface. The mass of the worms is evenl distributed along their bod length. The starting

More information

4452 Mathematical Modeling Lecture 13: Chaos and Fractals

4452 Mathematical Modeling Lecture 13: Chaos and Fractals Math Modeling Lecture 13: Chaos and Fractals Page 1 442 Mathematical Modeling Lecture 13: Chaos and Fractals Introduction In our tetbook, the discussion on chaos and fractals covers less than 2 pages.

More information

7. TURBULENCE SPRING 2019

7. TURBULENCE SPRING 2019 7. TRBLENCE SPRING 2019 7.1 What is turbulence? 7.2 Momentum transfer in laminar and turbulent flow 7.3 Turbulence notation 7.4 Effect of turbulence on the mean flow 7.5 Turbulence generation and transport

More information

Conservation of Linear Momentum for a Differential Control Volume

Conservation of Linear Momentum for a Differential Control Volume Conservation of Linear Momentum for a Differential Control Volume When we applied the rate-form of the conservation of mass equation to a differential control volume (open sstem in Cartesian coordinates,

More information

Magnetic Reconnection in Laboratory, Astrophysical, and Space Plasmas

Magnetic Reconnection in Laboratory, Astrophysical, and Space Plasmas Magnetic Reconnection in Laboratory, Astrophysical, and Space Plasmas Nick Murphy Harvard-Smithsonian Center for Astrophysics namurphy@cfa.harvard.edu http://www.cfa.harvard.edu/ namurphy/ November 18,

More information

Special topic JPFR article Prospects of Research on Innovative Concepts in ITER Era contribution by M. Brown Section 5.2.2

Special topic JPFR article Prospects of Research on Innovative Concepts in ITER Era contribution by M. Brown Section 5.2.2 Special topic JPFR article Prospects of Research on Innovative Concepts in ITER Era contribution by M. Brown Section 5.2.2 5.2.2 Dynamo and Reconnection Research: Overview: Spheromaks undergo a relaxation

More information

The nature of separator current layers in MHS equilibria. I. Current parallel to the separator

The nature of separator current layers in MHS equilibria. I. Current parallel to the separator A&A 573, A44 (2015) DOI: 10.1051/0004-6361/201424348 c ESO 2014 Astronomy & Astrophysics The nature of separator current layers in MHS equilibria I. Current parallel to the separator J. E. H. Stevenson,

More information

2.5 CONTINUITY. a x. Notice that Definition l implicitly requires three things if f is continuous at a:

2.5 CONTINUITY. a x. Notice that Definition l implicitly requires three things if f is continuous at a: SECTION.5 CONTINUITY 9.5 CONTINUITY We noticed in Section.3 that the it of a function as approaches a can often be found simpl b calculating the value of the function at a. Functions with this propert

More information

Available online at ScienceDirect. Procedia Engineering 90 (2014 )

Available online at   ScienceDirect. Procedia Engineering 90 (2014 ) Available online at.sciencedirect.com ScienceDirect Procedia Engineering 9 (14 383 388 1th International Conference on Mechanical Engineering, ICME 13 Effects of volumetric heat source and temperature

More information

Scaling of Magnetic Reconnection in Collisional and Kinetic Regimes

Scaling of Magnetic Reconnection in Collisional and Kinetic Regimes Scaling of Magnetic Reconnection in Collisional and Kinetic Regimes William Daughton Los Alamos National Laboratory Collaborators: Vadim Roytershteyn, Brian Albright H. Karimabadi, Lin Yin & Kevin Bowers

More information

Particle acceleration in stressed coronal magnetic fields

Particle acceleration in stressed coronal magnetic fields To be submitted to ApJ Letters Particle acceleration in stressed coronal magnetic fields R. Turkmani 1,L.Vlahos 2, K. Galsgaard 3,P.J.Cargill 1 and H. Isliker 2 ABSTRACT This letter presents an analysis

More information

Creation and destruction of magnetic fields

Creation and destruction of magnetic fields HAO/NCAR July 30 2007 Magnetic fields in the Universe Earth Magnetic field present for 3.5 10 9 years, much longer than Ohmic decay time ( 10 4 years) Strong variability on shorter time scales (10 3 years)

More information

Figure 1 Correlation diagram for BeH 2

Figure 1 Correlation diagram for BeH 2 Self-Stud Problems / Eam Preparation revise our computational chemistr workshop from last ear: http://www.huntresearchgroup.org.uk/teaching/ear1_lab_start.html o make sure ou have checked that the molecule

More information

LAB 05 Projectile Motion

LAB 05 Projectile Motion LAB 5 Projectile Motion CONTENT: 1. Introduction. Projectile motion A. Setup B. Various characteristics 3. Pre-lab: A. Activities B. Preliminar info C. Quiz 1. Introduction After introducing one-dimensional

More information

Hurricane Modeling E XPANDING C ALCULUS H ORIZON

Hurricane Modeling E XPANDING C ALCULUS H ORIZON Februar 5, 2009 :4 Hurricane Modeling E XPANDING THE Sheet number Page number can magenta ellow black C ALCULUS H ORIZON Hurricane Modeling... Each ear population centers throughout the world are ravaged

More information

Vector Calculus Review

Vector Calculus Review Course Instructor Dr. Ramond C. Rumpf Office: A-337 Phone: (915) 747-6958 E-Mail: rcrumpf@utep.edu Vector Calculus Review EE3321 Electromagnetic Field Theor Outline Mathematical Preliminaries Phasors,

More information

DIGITAL CORRELATION OF FIRST ORDER SPACE TIME IN A FLUCTUATING MEDIUM

DIGITAL CORRELATION OF FIRST ORDER SPACE TIME IN A FLUCTUATING MEDIUM DIGITAL CORRELATION OF FIRST ORDER SPACE TIME IN A FLUCTUATING MEDIUM Budi Santoso Center For Partnership in Nuclear Technolog, National Nuclear Energ Agenc (BATAN) Puspiptek, Serpong ABSTRACT DIGITAL

More information

THE DYNAMICS OF THE GRAVITATIONAL CAPTURE PROBLEM

THE DYNAMICS OF THE GRAVITATIONAL CAPTURE PROBLEM THE DYNAMICS OF THE GRAVITATIONAL CAPTURE PROBLEM Ernesto Vieira Neto Faculdade de Engenharia de Guaratinguetá - UNESP e-mail: ernesto@feg.unesp.br Antônio Fernando Bertachini de Almeida Prado Instituto

More information