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

Size: px
Start display at page:

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

Transcription

1 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 of Mathematics and Statistics, Universit of St. Andrews, St. Andrews, Fife, KY6 9SS, Scotland, UK b Theoretische Phsik IV, Ruhr-Universiteit, D-78, Bochum, German (Received 6 Februar ; In final form 7 Ma ) Magnetic reconnection at a three-dimensional null point is the natural etension of the familiar two-dimensional X-point reconnection. A model is set up here for reconnection at a spiral null point, b solving the kinematic, stead, resistive magnetohdrodnamic equations in its vicinit. A stead magnetic field is assumed, as well as the eistence of a localised diffusion region surrounding the null point. Outside the diffusion region the plasma and magnetic field move ideall. Particular attention is focussed on the wa that the magnetic flu changes its connections as a result of the reconnection. The resultant plasma flows are found to be rotational in nature, as is the change in connections of the magnetic field lines. Kewords: Magnetic reconnection; Magnetohdrodnamics; Magnetic flu; Magnetic null points INTRODUCTION Magnetic reconnection is a fundamental process in man areas of plasma phsics, whereb the magnetic field, B, becomes restructured. When null points are present the global topolog of the field changes. Our ideas on how this restructuring occurs come mostl from the well-studied case of reconnection in two dimensions. In two dimensions, reconnection occurs at hperbolic null points of the magnetic field (see, e.g. Priest and Forbes,, for a review), commonl known as X-points (see Fig. ). A plasma flow transports magnetic flu towards the X-point, where the reconnection takes place, and the flow then transports the reconnected magnetic flu awa from the X-point. In terms of magnetic field lines, the process of reconnection involves a pair of field lines being brought in from two quadrants on opposite sides of the null. At the X-point each of these field lines breaks, when the lie along the separatrices of the field. The are then rejoined and move out in the other two quadrants of B. The result is that the field line footpoints are pair-wise differentl connected when the leave the reconnection region. *Corresponding author. davidp@mcs.st-and.ac.uk ISSN 9-99 print: ISSN 9-9 online ß Talor & Francis Ltd DOI:.8/997

2 8 D.I. PONTIN et al. FIGURE Two-dimensional reconnection at an X-point. The thin lines are magnetic field lines and the bold arrows indicate the direction of the plasma flow. Magnetic reconnection is a fundamentall non-ideal process; in an ideal plasma, magnetic field lines maintain their identit for all time, and are said to be frozeninto the plasma. The non-idealness ma be the result, for eample, of a non-zero resistivit,, in which case, assuming no other non-ideal effects are important, the process satisfies Ohm s law in the form E þ vtb ¼ J: ðþ In order to investigate the evolution of magnetic flu it is useful to define a flu transporting velocit w (Hornig and Schindler, 996; Hornig and Priest, ) which satisfies E þ wtb ¼, ðþ which is possible in two dimensions since the electric field, E, is alwas perpendicular to B. Note that for reconnection to take place, the flu transporting velocit w must become singular at the null point, which is a signature of the breaking of the field lines (Hornig, ) and the subsequent discontinuit in the mapping of their endpoints. B comparison with an ideal Ohm s law, we can consider w to be a flow within which the magnetic flu is frozen. The component of w perpendicular to B can be found from w? ¼ ETB=B : ðþ If we assume that the non-ideal term on the right-hand side of Eq. () is localised within a finite region, D, about the null point, then outside D, w coincides with the plasma velocit perpendicular to B, v?. The situation in three dimensions is much more complicated. In general, for reconnection in three dimensions, EEB (or JEB) is non-zero within a finite region D, and hence in general no unique flu-conserving velocit eists, or in other words there is no unique field line velocit for field lines which thread D (for a proof, see Hornig and Schindler, 996; Priest et al., ). Nonetheless, it is still possible to stud the evolution of magnetic flu and field lines under certain circumstances. Consider the case of a resistive non-ideal term J, which is localised within some diffusion region, D. We consider a finite region D as the generic situation for astrophsical plasmas since

3 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT 9 these plasmas have etremel high magnetic Renolds numbers, and dissipation is enhanced in well localised regions, for eample, when micro instabilities form in a thin current sheet. If no closed magnetic field lines eist within D, then we can still follow the motion of individual field lines from each end, since we know that in the ideal region on either side of D the must remain attached to the same plasma elements for all time. Suppose the surface of D is split into two parts, through one of which magnetic flu enters D, and through the other of which it leaves. Since each field line is anchored twice in the ideal environment, once on either side of the non-ideal region, one can follow the motion of the field lines b tracing them through space from either of these two sets of footpoints. B reference to the ideal environment then, it is possible to define a velocit with which the field lines passing into D move, sa w in, and another velocit w out at which the field lines passing out of D move. In the stationar case, these two velocities can be calculated throughout space b mapping the electric potential from each set of footpoints along the field lines. This leads us to the mathematical epressions given in Eqs. (6) and (7). These two (pseudo-)field line velocities must each be identical to v? on the relevant section of the surface of D, but in contrast to the two-dimensional case, the are not identical to each other inside D, nor are the identical to v? on their continuations through D. This is a manifestation of the non-eistence of a unique field line velocit, w, as stated above. The result is that, following field lines with w in and w out, respectivel, the field lines seem to split as soon as the are transported into the diffusion region, and inside D the continuall change their connections. Reconnection can occur in three dimensions either at a null point or in the absence of a null point (Schindler et al., 988; Lau and Finn, 99; Priest and Forbes, ). The nature of the field line splitting, and subsequent restructuring of the magnetic flu, for reconnection in a simple magnetic structure with no null point has been discussed in general b Priest et al. (), and in more detail b Horing and Priest (). Here we stud instead the kinematic problem at a three-dimensional null point. We find that the induction equation implies that such reconnection is profoundl different from two-dimensional X-point reconnection. The implications for further stud are addressed in the conclusion. In Section, we describe the structure of three-dimensional null points as well as describing ideal field line behaviour in their vicinit. In Section, the equations solved in our model are given, as well as the assumptions made, and we detail our method of solution. The elementar solution is given in Section, before we describe the result of adding a phsicall relevant ideal flow in Section 5. The eistence of perfectl reconnecting flu tubes is discussed in Section 6, where the effect of adding a simple time-dependence to the model is described. We give our conclusions in Section 7. STRUCTURE OF D NULL POINTS AND IDEAL BEHAVIOUR The nature of reconnection at a three-dimensional null point is of particular interest since it is the three-dimensional generalisation of an X-point. Three-dimensional null points are also of crucial importance in the topolog and interaction of comple fields on the Sun. The are found in abundance in the solar corona (see e.g. Brown and Priest, ; Longcope et al., ), where their associated separatrices

4 D.I. PONTIN et al. z spine fan FIGURE Basic structure of a three-dimensional null point. and separators are thought to be likel candidates for sites of coronal heating (Longcope, 996; Antiochos et al., ; Priest et al., ). There is also evidence that null point reconnection ma act as a trigger for at least some solar flares (Fletcher et al., ). The local structure of the magnetic field around a three-dimensional null point is shown in Fig.. The skeleton of the null point is made up of a pair of field lines directed into (or out of ) the null from opposite directions, known as the spine, and a famil of field lines which are directed out of (or into) the null ling in a surface, known as the fan plane (Priest and Titov, 996). A general mathematical formalism is given b Parnell et al. (996), who classif nulls depending, amongst other things, on the size of the current, J, and its direction with respect to the spine ais and fan plane. If the current is zero then the null point is known as potential. When the current is directed onl parallel to the spine (J ¼ J k ), the fan and spine are perpendicular, and the field lines in the fan form a spiral structure (Parnell et al., 996). When the current is directed onl perpendicular to the spine (J ¼ J? ), the spine and fan are no longer perpendicular. In general, when the current has components in both directions, both of these effects are present, as well as further characteristics, depending on the relative magnitudes of J k and J?. The kinematics of stead reconnection at a three-dimensional null point have been studied previousl b Priest and Titov (996). The start off b discussing the ideal behaviour in the vicinit of the simple potential magnetic null given b B ¼ ð,, zþ: ðþ The reconnection is classified as one of two tpes near an isolated null point, termed spine reconnection and fan reconnection. Reconnection associated with a separator, a special field line which joins two null points, is also discussed. Due to the fact that the configuration considered is ideal, to achieve reconnection, the plasma velocit is necessaril singular at the null, and the field line mapping is discontinuous. During spine reconnection a flow is imposed across the fan (z ¼ ) resulting in singularities in E and v at the spine ( ¼ ¼ ). In fan reconnection, the flow is imposed across

5 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT the spine resulting in singularities in E and v in the fan plane. The effect of adding nonpotential and diffusive terms is then considered in a preliminar manner. We aim here to investigate the structure of reconnection when the null point is nonpotential, with a current parallel to the spine, where a localised diffusion region is included in order to get a realistic model with no singularities in an phsical quantities. It is instructive to seek insight into the structure of the highl comple process of three-dimensional reconnection b considering solutions to a reduced set of the MHD equations. We follow the method of Hornig and Priest () in adopting the kinematic approimation, b solving the induction equation and Mawell s equations, though not solving the equation of motion. In a dnamical situation we would epect to start from an initial field, which then forms a current sheet (diffusion region) at which reconnection takes place. The wa in which a current sheet ma form b the collapse of such null points is discussed b Parnell et al. (997) and Mellor et al. () as well as b Klapper et al. (996) and Bulanov and Sakai (997). It should be noted, however, that as in two dimensions, reconnection ma be initiated in man different was (see e.g. Priest and Forbes, ), such as b driving from boundaries, or as a result of instabilities of man different tpes, as well as b null point collapse (following response to eternal boundar motions). Our investigation here is independent of the initiation mechanism. THE MODEL We seek a solution of the kinematic, stead, resistive MHD equations given b E þ vtb ¼ J, JTE ¼, ð5; 6Þ JEB ¼, JTB ¼ J: ð7; 8Þ The non-ideal term on the right-hand side of Eq. (5) is assumed to be localised, for the reasons described in Section. We investigate the behaviour in the vicinint of a simple spiral null point, where J lies parallel to the spine. In the future, we will go on to consider the case where J is perpendicular to the spine. In general the field in the vicinit of our spiral null point can be written (Parnell et al., 996) as B ¼ B j, þ j, z, ð9þ where B and j are constants, such that J ¼ðB j= Þ^z (from Eq. (8)) is directed along the z-ais, which is coincident with the spine. Due to the clindrical smmetr of the field, it simplifies matters to work in clindrical polar coordinates ðr,, zþ, in which B has the form B ¼ B R, jr, z : ðþ It is crucial for the following analsis to be performed analticall that we are able to find analtical equations describing the field lines in terms of some initial starting

6 D.I. PONTIN et al. coordinates,. For B defined as in Eq. (), this can be done b integrating dxðsþ ds ¼ BðXðsÞÞ ðþ to find X ð, sþ, given b Eq. (), as R ¼ R ep ðb sþ, ¼ þ B jrs, z ¼ z ep ð B sþ: ðþ Note that the parameter s does not denote the distance, dl, along a field line, which is instead given b dl ¼jBjds: ðþ From Eq. (6) we can see that E can be written as the gradient of some scalar, sa, so that Eq. (5) becomes J þ vtb ¼ J: ðþ A solution to this equation for given B ma be found as follows. Firstl, since we require our non-ideal term to be localised and since J is constant, we prescribe a localised resistivit,. The component of Eq. () parallel to B is ðjþ k ¼ J k, which ma be integrated along field lines to give Z Z ¼ J k dl þ ¼ JEBds þ : ð5þ Thus, if we can prescribe some function ¼ ð, sþ in such a wa that, having substituted Eq. () into B and J to find B ð, sþ and J ð, sþ, Eq. (5) is integrable, then we can deduce ð, sþ. From here it is possible to substitute the inverse of Eq. () to find ðþ. Then the electric field, E, and the component of the plasma velocit perpendicular to B, v?, can be found from E ¼ J ð6þ and v? ¼ ðe JÞTB=B : ð7þ Prescribing a phsicall reasonable profile for ðþ we can obtain an epression for in terms of the field line coordinates ð, sþ with the help of the coordinate transformations (Eq. ()). This epression can then be used for the integration (Eq. (5)). In order to have a unique coordinate transformation!ð, sþ, we need to choose the initial points on surfaces such that each field line passes through these surfaces eactl once. Two obvious choices which we will use in the following discussions are the planes z ¼, or a clindrical surface such as R ¼.

7 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT It is now necessar to choose ðþ in such a wa that the integral in Eq. (5) can be performed analticall. One analticall integrable form for ðþ is a piecewise polnomial function, such as ( ðr=aþ ¼ ðz=bþ R < a, z < b ; ; otherwise; ð8þ where, a and b are constant and is the value of the resistivit,, at the null point. This form of gives a clindrical diffusion region, of radius R ¼ a, sa, etending in the z-direction to b. We are choosing this shape for simplicit, and aim to consider other shapes in the future. is continuous and smooth everwhere. To proceed we need to perform the integration given b Eq. (5). In order to do this we must choose in which direction along the magnetic field lines to integrate. That is, we ma choose either to set s ¼ on some surface of R ¼ R (where R is a constant, R >a) and integrate in towards the null point and thus through D, or we ma integrate down and up towards the null from z ¼ z and z ¼ z, respectivel (constant z >b), setting s ¼ on these surfaces for each half-space. In the latter case the starting potentials ( )at z ¼z must be chosen such that is continuous and smooth at the fan plane (z ¼ ). However, the choice between these two directions of integration is irrelevant provided we consider our model with respect to some chosen eternal/boundar conditions, equivalent to imposing some on one boundar. The results from each case then are equivalent, and so we choose here to describe the result of setting s ¼ on z ¼z, constant, and point out an significant differences for the other case when the occur. B the method described above, E ð Þcan be found. However, it turns out that for the choice of given in Eq. (8), E is singular in the fan (z ¼ ). The reason is that is not sufficientl flat near the null point, where the diverging field lines make the integration of ver sensitive to an variations of. To obtain a smooth (and therefore phsicall acceptable) E, we find that the power of the variables in Eq. (8) must be greater than, and so take, for simplicit, ( ðr=aþ ¼ 6 ðz=bþ 6 R < a, z < b ; otherwise; ð9þ where, a and b have the same phsical meanings as before. This form for has essentiall the same structure as that given b Eq. (8). It is now possible, via the method described at the beginning of this section, to calculate E and v?. The analtical epressions for these are too length to present here, but can be calculated using a smbolic computation program. The resulting solution, described in detail in the following section, gives, in a sense, a local rearrangement of the flu within an envelope of field lines enclosing the diffusion region, D, see Fig.. The rearrangement is local in the sense that onl changes on field lines which pass through D (see Eq. (5)), and thus in a region of space threaded eclusivel b field lines which have not passed through D, is constant, and Eqs. (6) and (7) impl that E and v? are zero.

8 D.I. PONTIN et al..5.5 z.5.5 FIGURE Field lines on the boundar of the envelope enclosing the diffusion region (clinder), showing the region of influence of the local solution. Now, for a given magnetic field, Ohm s law (Eq. ()) ma be decomposed into an ideal component (Eq. ()) and a non-ideal component (Eq. ()) as follows J non-id þ v non-idtb ¼ J; J id þ v id TB ¼ : ðþ ðþ We have the freedom to add an ideal flow to the non-ideal solution since we do not solve the momentum balance equation here, which would otherwise determine the ideal part of the flow. We can thus add an ideal flow to our local solution b taking id to be our in Eq. (5). Note that id should be constant with respect to the integration in Eq. (5), i.e. id ¼ id ð Þ. The perpendicular component of the ideal flow v id? ma then be calculated, b taking the cross-product of Eq. () with B, as v id? ¼ J id TB=B : ðþ We ma thus add an ideal flow to transport magnetic flu into and out of the local envelope shown in Fig., allowing us to see the global effect of the restructuring of the magnetic flu b the reconnection process. This will be discussed in Section 5, but first let us consider the elementar solution. ELEMENTARY SOLUTION. Induced Flows We eamine here the nature of the solution with id ¼, i.e. just the local behaviour of the flu envelope enclosing D with no etra ideal flow. All phsical quantities are completel smmetric about z ¼, and we will therefore describe the results onl for z>. Choosing to integrate Eq. (5) from z ¼ z we automaticall start with constant for z>b. Hence the electric field and plasma velocit are zero for z>b. The velocit for

9 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT 5 z<b is a rotation within the flu envelope. (For integration from R ¼ R, the plasma velocit, v, vanishes for R >a, and we have a rotation within the remainder of the flu envelope.) For the purposes of illustration of the results, it is at this stage convenient to add a component of v parallel to B such that v z ¼. This is achieved b defining v ¼ v? ðv?z =B z ÞB: ðþ Our freedom to do this comes from the fact that Eq. () determines onl the perpendicular component of v, since it is the part that affects the behaviour of the magnetic flu, and so for our purposes the parallel component is arbitrar. The resulting flow pattern of v in a plane of constant z is shown in Fig. a. The radial component, as well as b definition the z-component, of v is zero, so we have purel rotational flow, and the wa that this varies with radius is shown in Fig. b. Note that here the angular plasma velocit is strongest in a ring centred on the spine. Note also that in the z ¼ plane the fan field lines rotate like a solid bod, as does the plasma outside the diffusion region. The source of the rotational flows can be eplained as follows. We consider the case where is integrated from z ¼ z, and the argument can be easil adapted to the reverse integration. Consider the potential drop along sections of the loop illustrated in Fig. 5. L andl are radial lines in planes z ¼ b and z < b, respectivel, while L is a field line on the surface of the envelope of flu threading D, and L lies along (a).5.5 (b).5.5 R FIGURE (a) Vectors of the plasma flow v, along with a projection of the magnetic field lines in the plane z ¼ :, for the parameters B ¼, a ¼, b ¼, ¼, j ¼. The corresponding radial variation of the plasma velocit v (black line) and field line velocit w out (gre). L L L L FIGURE 5 Closed loop made up of line sections. L and L are radial lines in planes z ¼ b and < z < b respectivel. L is a field line ling on the surface of the flu envelope enclosing D, and L lies along the spine (R ¼ ).

10 6 D.I. PONTIN et al. the spine of the null. The potential drop around an closed loop must be zero. The potential drop along lines L andl must be zero, as L lies at z b and L lies on the boundar of the envelope, and so ¼ all along them. Thus or L þ L ¼, L ¼ ð spine Þ 6¼, ðþ where spine is the value of at the verte of L andl, which must be different from since E is non-zero along the spine (EEB ¼ JEB 6¼ on spine). Since there is a potential drop along L there must also be a non-zero electric field along it. This electric field induces a plasma flow perpendicular to such a radial line, i.e. a rotational flow. This rotation has the same sense for z> and z<, and has maimum magnitude in the z ¼ plane. Note that this argument is completel independent of the particular profile of within D.. Reconnection Rate It is possible to calculate a reconnection rate for the flu in this reconnection process, although it is important to note that this has a ver different phsical meaning from the concept of a reconnection rate in two-dimensional reconnection. In two dimensions, flu is cut and rejoined at the null point, and the reconnection rate gives a measure of the amount of flu that undergoes this process in a given time. However, in three dimensions we need a different definition since we have a localised flu envelope within which all of the flu continuall changes its connections, so during an arbitraril short length of time ever field line is reconnected (ecept, for smmetr reasons, the spine field line). Considering just the flu reconnected in the half-space z >, we define, b close analog to Hornig and Priest (), the reconnection rate, F, as the integral over the parallel electric field along the spine ais, F ¼ Z E k R¼ z¼ dl ¼ ðr ¼, z ¼ bþ ð R ¼, z ¼ Þ ¼ 7 9 B j b: ð5þ To obtain some idea of the meaning of this quantit, consider the difference between the velocities of the field lines anchored in the surfaces, z ¼b and R ¼ a, ofd through which flu passes in and out. Since the velocities w in=out must match the plasma velocit on the relevant boundar of D, the are given b w in=out ¼ r in=out B=B : ð6þ Assuming B >, we can now identif the surface through which flu enters D as z ¼ b, and the surface through which flu leaves it as R ¼ a, namel, w in ¼ J z¼b TB=B, w out ¼ J R¼a TB=B : ð7þ

11 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT 7.5 z.5 FIGURE 6 Flu surfaces of constant radius (for given z), within which field lines periodicall eactl reconnect with themselves. For eample, the highlighted (black) field line will split in the rotational flow, with the top half remaining fied, while the bottom half reconnects with each of the gre field lines until eventuall being reconnected again into the configuration shown after performing a rotation of radians. Now, ¼ on z ¼ b, and hence J z¼b ¼ and w in ¼, so field lines passing in through the top of D remain fied and stationar there. Due to the rotational nature of v, w out is also rotational, leading to a rotational mismatching between w in and w out. The value of F, given b Eq. (5), provides an idea of the maimum difference between the rate of rotation of the inward flu bundle and outward flu bundle, or the maimum rate of relative slippage (see Hornig and Priest,, for a further pedagogic eample). From Fig. b it can be seen that the outward bundle of field lines rotates approimatel like a solid bod close to the spine, with the rotation falling off to zero at the edge of the flu envelope. As mentioned above, w ¼ w out w in, the rate of slippage between the inward and outward bundles of field lines, is purel rotational, so that it has a -component onl. Thus field lines are continuousl reconnected in shells of constant radius (for a given value of z) onl. These shells have the same three-dimensional shape as, and are concentric with, our flu envelope, see Fig. 6. An initial field line which splits into two will be periodicall eactl reconnected with itself, ever time the half embedded in R ¼ a performs a full rotation of radians. Note, however, that this period is different for each shell, since it is not a rigid rotation. For this reason, if we consider a flu tube within the envelope with a finite radial etent, there will be no periodic return to the initial state. It is important to note the implications the rotational slippage has for helicit production. If we imagine that the small flu tube within our flu envelope is closed somewhere far from D, then we can see that the relative rotation of the two ends of the tube would act to twist up the tube and thus act as a source of self-helicit with respect to an initiall untwisted tube. 5 COMPOSITE SOLUTIONS As discussed in Section, we ma impose an ideal flow upon the solution described in the previous section, as shown in Eqs. () and (). We would like to choose an

12 8 D.I. PONTIN et al. ideal flow which shows the global effect of the local rotational slippage behaviour b transporting magnetic flu into and out of the local flu envelope. For this reason, we choose to impose a stagnation-tpe ideal flow. Stagnation flows are phsicall relevant flows to choose as the ma perform the localisation of the quantities contained in the non-ideal term in Eq. (5) (Priest and Forbes, ; Hornig and Priest, ), and are common in reconnection solutions, such as Craig and Fabling (996). The stagnation flow is chosen in such a wa as to satisf Eq. () b imposing a suitable id ð, Þ on the surface z ¼ z, and then substituting the inverse of the field line equations () to obtain id ð,, zþ. The equivalents of Eq. (6) and (7) can then be used to find E id and v id?, respectivel. Again, for ease of analsis, we choose to set ðv id? Þ z ¼, via Eq. (), to obtain v id. We choose to take id ð, Þ ¼, ð8þ where is a constant. The resulting flow, v id, takes the form of a stagnation-point flow, with separatrices coincident with the - and -aes in the plane z ¼ z. For z 6¼ z, the flow separatrices are rotated with respect to this configuration, due to the spiralling of the magnetic field lines. The total flow, obtained b adding this ideal flow to the elementar solution, and given b v þ v id, has the same stagnation-tpe structure outside the enclosing flu envelope, but inside we have a superposition of X-tpe and O-tpe flows. Whichever of these flows dominates is dictated b the nature of near the spine, R ¼. If we consider all other parameters fied, there is a critical value of, namel ¼ crit, at which the transition from O-tpe to X-tpe flow takes place. This can be determined b eamining the total at small R, which (in cartesian coordinates) takes the form ¼ þ þ þ þ þ O,, ð9þ where ¼ B j 9b z 7z þ 6z 6 b 6 9b, ¼ 9B j 5a z, z ¼ cos sin, z ¼ j ln z ; z ¼ cos sin z : ðþ In a plane of constant z, changes from a local maimum to a saddle point, and thus the flow changes from O-tpe to X-tpe, when z ¼ :

13 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT 9 Substituting in the above epressions for, and and rearranging for we find that crit ¼ 8B j z 5a : ðþ For > crit, the flow is of X-tpe at the spine ais, whereas for < crit it is O-tpe. Note that crit is independent of z, so the flow tpe is the same for all z for a given value of. 5. The Case u >u crit For > crit, the stagnation flow dominates the rotational flow of the elementar solution everwhere, and hence v, w in and w out all have a basic X-tpe structure. In order to analse the effect the reconnection process has on rearranging the flu, we consider the mismatching of the two flu velocities w in and w out. The flow lines of these velocities are coincident with the contours of constant in and out, respectivel. For clarit we eamine the mismatching of these contours, and hence the flu velocities, in the plane z ¼ b, without loss of generalit. The two sets of contours are shown in Fig. 7. Note that the flow w in is eactl the ideal plasma velocit, v id, since the associated elementar solution from the previous section is zero on z ¼ b. Note also that in the plane z ¼ b, the boundar of the flu envelope associated with the elementar solution coincides with the boundar of the diffusion region, at R ¼ a. The superposition of the flow lines of w in and w out is shown in Fig. 8a, which ma be understood as follows. Consider a magnetic field line in an inflow region outside the diffusion region, whose intersection with the chosen plane, z ¼ b, lies on one of the sketched flow lines. Outside D, the two sets of flow lines coincide (with each other and with v), and the field line moves ideall. Once the field line is transported into D, the flu velocities w in and w out are no longer the same, and so we ma choose to follow either the field line anchored in the ideal region above D, which moves at w in, or follow the field line anchored in w out. Plotting both motions the field line seems to split, as shown b the splitting of the flow lines. There are three distinct tpes of behaviour of the magnetic flu, which occur in different regions of the flows. These regions are separated b the separatrices of the w-flows, as well as those flow lines which just touch (but do not enter) D, all of (a).5.5 (b).5.5 FIGURE 7 Flow lines in the plane z ¼ of the field line velocities w in (a) and w out (b). The adopted parameter values are B ¼, a ¼, b ¼, ¼, j ¼, ¼ > crit.

14 D.I. PONTIN et al III (a).5.5 (b) I II.5.5 II I FIGURE 8 (a) The superposition of the two sets of flow lines shown in Fig. 7, highlighting the mismatching, and (b) the regions of different reconnective behaviour, distinguished b separatrices of w in (gre) and w out (black), as well as flow lines just touching the surface of D (dashed). which are shown in Fig. 8b. Regions I show ideal behaviour everwhere. Here w in and w out coincide, and so field lines alwas remain connected and frozen to the plasma. In regions II, the flow lines split inside D, and so an initiall unique field line splits, with each footpoint becoming differentl connected. Notice, however, that although an two flow lines separate when the enter D, the same two flow lines alwas come back together when the leave D. We can therefore think of these regions as slippage regions, since, although in general the two halves of the initial field line will take different times to pass through D, and will hence not rejoin upon leave D, the do move awa from the reconnection region along the same flow line. Hence after both halves of the field line have left D, their separation remains constant in time. Regions III are quite different. Here again there is a splitting of flow lines, and thus field lines, at the edge of D. In contrast to regions II, however, the flow lines in this case never rejoin, and in fact head off in opposite directions. Hence after we leave D each footpoint of our initial field line is now connected to a field line from a topologicall distinct region of magnetic flu. Regions III, then, can be thought of as more of a classical tpe of reconnection region, with the crucial characteristic being that initiall joined field line footpoints continue to move awa from each other for all time after leaving D. As, and hence the strength of the ideal flow, is decreased, these classical reconnection regions grow in width, until we reach ¼ crit. 5. The Case u <u crit When < crit, the rotational flow dominates w out near the spine, whereas w in retains the X-tpe structure, as it still coincides with v id. The two sets of flow lines and their superposition are shown in Figs. 9 and a. Again the different tpes of behaviour can be most clearl distinguished b studing the separatrices of these flows, which are shown in Fig. b. Regions I, II and III have essentiall the same characteristic behaviours as before. Notice, however, that regions III where the classical flu separation occurs are now wider than when > crit (if all other parameters are fied). In addition we now have a region, marked IV in Fig. b, where the nature of the flu

15 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT (a).5.5 (b).5.5 FIGURE 9 Flow lines in the plane z ¼ of the field line velocities w in (a) and w out (b). The chosen parameters are B ¼, a ¼, b ¼, ¼, j ¼, ¼ < crit..5.5 IV.5.5 (a).5.5 (b) I II III II III.5.5 FIGURE (a) The superposition of the two sets of flow lines shown in Fig. 9, highlighting the mismatching, and (b) regions of different reconnective behaviour, distinguished b separatrices of w in (gre) and w out (black), as well as flow lines just touching the surface of D (dashed). reconnection is different again. In this region the flow lines of w out are closed, and so following a field line anchored in this flow, we find that it simpl rotates round and round, never leaving the region or the local flu envelope. So we have a continuousl rotating flu bundle moving at w out, which reconnects with a succession of different field lines, which are swept into and then out of the reconnection region at w in. Note that the reconnection rate for both of the composite solutions described in this section is eactl the same as that given in Eq. (5) for the elementar solution, since id ¼ when R ¼, and so the calculation is unaffected. This reconnection rate now, however, summarises the sum of man different effects. Lastl, note that the above analsis would follow through in eactl the same wa had we chosen the option initiall of integrating from R ¼ R. The onl difference would be that flow lines of w in would become flow lines of w out and vice-versa. 5. Reconnection of Flu Tubes To visualise the effect the mismatching of the field line velocities has on the reconnection of flu tubes, we now describe two eamples. In each case, field lines are integrated from four arbitrar cross-sections chosen smmetricall about the spine such that initiall we have two unique flu tubes on opposite sides of the diffusion region. The

16 D.I. PONTIN et al. cross-sections are chosen so that the never pass into the diffusion region, and hence we can identif a set of field lines which remains frozen into these cross-sections for all time, defining our flu tubes. The resulting motion of the flu tubes is plotted, although we stop the field line integration at a chosen point to see more clearl what is happening. When the flu tube cross-sections are chosen to lie in region II, the resulting flu tube behaviour is a slippage, as described in Section 5., and shown in Fig.. We see that the flu tubes slip apart as the enter D, but the two sections of each initial flu tube leave the vicinit of the reconnection process in the same direction. The degree of slippage depends on the initial positions of the cross-sections, and the size of. The evolution of flu tubes whose cross-sections lie in regions III is shown in Fig.. Now the two sections of each flu tube flip around the spine in opposite directions after splitting. The then leave the diffusion region in opposite directions, as described in Section 5.. Notice, however, that the four flu tubes formed during the splitting process never rejoin cross-wise to form two unique flu tubes again as the do in two-dimensional reconnection. The ma share a few common field lines, although this need not necessaril be the case, depending on eactl where in region III the initial cross-sections are chosen. Z Z X X Y Y Z Z X X Y Y FIGURE Evolution of a pair of flu tubes integrated from cross-sections ling in region II of the w-flows. As the enter the diffusion region each tube splits into two parts, which slip apart, but on leaving D the move off in the same direction.

17 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT Z Z X X Y Y Z Z X X Y Y FIGURE Evolution of a pair of flu tubes integrated from cross-sections ling in region III of the w- flows. As the tubes enter the diffusion region the split, with the two parts of each of the initial two tubes flipping around the spine in opposite directions. Notice in the final frame that after leaving D the four new tubes do not rejoin to form two unique tubes. 6 EXISTENCE OF PERFECTLY RECONNECTING FLUX TUBES AND TIME DEPENDENCE We now ask whether it is possible to choose a pair of initial flu tubes which will perfectl rejoin after reconnection, such that we have two unique tubes before reconnection and two unique cross-wise connected tubes after reconnection. We have seen in the previous section that this is not generall the case, but perhaps with the right choice of initial cross-sections we can achieve this situation. In two dimensions, things are relativel straightforward. If we choose to pick out one field line, in an inflow region of v outside D, then it is alwas possible to find a corresponding field line, b simple smmetr through the X-point, with which it will perfectl reconnect. That is to sa, if we label the two footpoints of field line g and h, and of field line g and h, then, if the field lines are chosen such that after reconnection g is connected to g, then h will alwas be connected to h (see Fig. a). So in two-dimensions there is a simple one-to-one reconnection of field lines, and hence flu tubes. In three dimensions this is not generall the case (Priest et al., ), i.e., if g becomes connected to g after reconnection then h will not be connected to h (see Fig. b). In this sense there is

18 D.I. PONTIN et al. (a) g h BEFORE (b) g h BEFORE g h g h g AFTER h g AFTER h h g h g h h FIGURE (a) The one-to-one reconnection of field lines in D. (b) Schematic picture of reconnection of field lines in D, for eample top view of reconnection in region III of the composite solution of Section 5. no one-to-one reconnection of field lines, so a given field line has no unique counterpart with which it becomes uniquel rejoined. Nevertheless, if we can find two finite sets of field lines which reconnect with each other then we ma still have perfect, or one-to-one, reconnection of these particular flu tubes. An iteration procedure for finding sets of field lines on either side of D which reconnect with each other is described in Hornig and Priest (). The procedure involves sequentiall tracking field lines as the reconnect, moving in the flows w in and w out. In fact, in the stationar case it turns out that the sets of field lines which reconnect with each other lie in surfaces (see Fig. a), and so there are no perfectl reconnecting flu tubes. We find that, if a simple time-dependence is introduced into, as in Eq. (), then perfectl reconnecting flu tubes can be found, as follows. Let ( ½ðR=aÞ 6 Š ½ðz=bÞ 6 Š ; R < a, z < b ; ¼ fðþ t ; otherwise; ðþ where fðþis t some arbitrar function of time onl, and is thus effectivel just a multiplicative constant in the calculation of and E described in Section. Hence JTE is still zero, and no etra magnetic field is induced. This time-dependence, then, shows up in, E, v and thus w in and w out. B the same argument, a time-dependence could also be added to the ideal flow. We will consider here the case where the ideal flow is still stead, and the diffusive process is localised in time via ft ðþ¼ep ð t =T Þ, ðþ where T is a constant which controls the time-scale of the localisation. This timedependence has little qualitative effect on the results described in the previous section, other than to localise the effect of the reconnection process in time.

19 KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT (a) (b) FIGURE Schematic picture of reconnection of magnetic field lines in (a) a stationar state and (b) a time-dependent state, where there is one-to-one reconnection of flu tubes but not field lines. In order to ensure numerical stabilit of the iteration process, we choose to add to the elementar solution a slightl different ideal solution to that described in the previous section. For the ideal potential, we choose id ¼ ep þ =, ðþ so that the ideal solution is approimatel the same as before near the diffusion region, but now the ideal velocit falls off with radius far awa from the reconnection region. The flow lines and separatrices of w in and w out associated with the new composite flow are shown in Fig. 5, at t ¼. We find that the result of adding the time dependence is that the flu surfaces of the stationar case close up to form flu tubes, as shown in Fig. b. Note that although these flu tubes do perfectl reconnect, there is still no one-to-one reconnection of field lines. For eample, in the left hand tube footpoint is connected to footpoint 6 after reconnection, whereas in the right hand tube footpoint is connected to footpoint 8. The mapping of the field lines in the reconnected flu tubes shows a rotation, with respect to a one-to-one correspondence. This signifies the production of twist, and hence a finite amount of self-helicit due to the rotation, consistent with the idea of the elementar solution as a helicit source as described in Section. The result of carring out the iteration procedure is that the field line footpoints that we obtain trace out closed curves, shown in Fig. 6. These curves represent the crosssections of perfectl reconnecting flu tubes in planes of constant z. Precisel what

20 6 D.I. PONTIN et al. (a) (b) FIGURE 5 (a) Flow lines of w in (gre) and w out (black) for the modified time-dependent flow for > crit and t ¼ and (b) the separatrices of these flows. (a).5.5 (b).5.5 (c).5.5 FIGURE 6 Perfectl reconnecting cross-sections in the time-dependent situation, in the plane z ¼ b. For the parameters a ¼, b ¼, B ¼, ¼, j ¼, ¼, and (a) T ¼, (b) T ¼ and (c) T ¼ 8. The gre lines are the separatrices of w out, while the separatrices of w in coincide with the - and -aes. cross-sections are traced out depends on the starting point for the iteration procedure, with these cross-sections being concentric for fied T. The effect of varing T, i.e. the localisation of the reconnection process in time, on the perfectl reconnecting flu tube cross-sections can be seen in Fig. 6. When the process is highl localised in time (T small) the cross-sections are fairl round, but as we increase T the cross-section becomes a thinner and thinner ellipse, whose major ais collapses towards a special time-smmetric flow line. When T is so large that we obtain a state which is numericall equivalent to the stead state, the iteration points (field lines) all lie along this flow line and we return again to a flu surface. 7 CONCLUSIONS We have described here a stead solution of the kinematic resistive MHD equations, which eists in the vicinit of a spiral null point of the magnetic field, with a diffusion term localised around the null. Of course there are man other questions that will need

21 to be answered before a full understanding of these processes can be obtained, such as the role of Lorentz forces in producing the current sheet and driving the reconnection. A rotational tpe of flu reconnection is found, similar to that described in Hornig and Priest () for reconnection in the absence of a null point. The reconnection of magnetic flu takes the form of a rotational slippage within an envelope of flu enclosing the diffusion region. We note that this rotational form of slippage is independent of the size and shape of the diffusion region. In order to stud the effect of the process on the global magnetic field structure, an ideal flow was added which transports flu into and out of the local flu envelope. This results in different behaviours for field lines frozen into different regions of the ideal flow. In one region in particular, the rearrangement of the flu has some similar characteristics to two-dimensional reconnection, where the two parts of an field line (mapped from initiall joined ends) separate, and the separation distance increases for all time. However, it is found that there is no simple one-to-one correspondence of reconnecting field lines after reconnection has occurred. As a result, there is also no splitting and one-to-one rejoining of flu tubes in the stead time-independent case. The result is that the re-ordering of flu b the reconnection process is much more complicated than at a familiar two-dimensional null point. In the future, we plan to set up a numerical eperiment for the full equations, including the equation of motion, and incorporating the invaluable insights that we have gained from this article. In particular, we shall calculate the flu motions w in and w out and will investigate whether the different tpes of kinematic reconnection that we have discovered here are realisable in the dnamic regime. Acknowledgments The authors would like to acknowledge financial support from the European Communit Human Potential Program under Contract No. HPRN-CT--5, PLATON. G.H. would like to thank the VW-Foundation for finanicial support and D.I.P. is grateful to the Carnegie Trust for a PhD Scholarship. References KINEMATIC RECONNECTION AT A MAGNETIC NULL POINT 7 Antiochos, S.K., Karpen, J.T. and DeVore, C.R., Coronal magnetic field relaation b null-point reconnection, Astrophs. J. 575, (). Brown, D.S. and Priest, E.R., The topological behaviour of D null points in the Sun s corona, Astron. Astrophs. 67, 9 6 (). Bulanov, S.V. and Sakai, J., Magnetic collapse in incompressible plasma flows, J. Phs. Soc. Jpn. 66,, 77 8 (997). Craig, I.J.D. and Fabling, R.B., Eact Solutions for stead state, spine, and fan magnetic reconnection, Astrophs. J. 6, (996). Fletcher, L., Metcalf, T.R., Aleander, D., Brown, D.S. and Rder, L.A., Evidence for the flare trigger site and three-dimensional reconnection in multiwavelength observations of a solar flare, Astrophs. J. 55, 5 6 (). Hornig, G., The geometr of reconnection, In: An introduction to the geometr and topolog of fluid flows (Ed. R.L. Ricca), pp. 95, Kluwer, Dordrecht (). Hornig, G. and Priest, E.R., Evolution of magnetic flu in an isolated reconnection process, Phs. Plasmas, 7 7 (). Hornig, G. and Schindler, K., Magnetic topolog and the problem of its invariant definition, Phs. Plasmas,, (996). Klapper, I., Rado, A. and Tabor, M., A Lagrangian stud of dnamics and singularit formation at magnetic null points in ideal three-dimensional magnetohdrodnamics, Phs. Plasmas, 8 8 (996).

22 8 D.I. PONTIN et al. Lau, Y.-T. and Finn, J.M., Three-dimensional kinematic reconnection in the presence of field nulls and closed field lines, Astrophs. J. 5, (99). Longcope, D.W., Topolog and current ribbons: A model for current, reconnection and flaring in a comple, evolving corona, Solar Phs. 69, 9 (996). Longcope, D.W., Brown, D.S. and Priest, E.R., On the distribution of magnetic null points above the solar photosphere, Phs. Plasmas,, (). Mellor, C. Titov, V.S. and Priest, E.R., Linear collapse of spatiall linear, three-dimensional, potential null points, Geophs. Astrophs. Fluid Dnam. 97, (). Parnell, C.E., Smith, J.M., Neukirch, T. and Priest, E.R., The structure of three-dimensional magnetic neutral points, Phs. Plasmas, (996). Parnell, C.E., Neukirch, T., Smith, J.M. and Priest, E.R., Structure and collapse of three-dimensional magnetic neutral points, Geophs. Astrophs. Fluid Dnam. 8, 5 7 (997). Priest, E.R. and Forbes, T.G., Magnetic reconnection: MHD theor and applications, Cambridge Universit Press, Cambridge (). Priest, E.R. and Titov, V.S., Magnetic reconnection at three-dimensional null points, Phil. Trans. R. Soc. Lond. A, 5, (996). Priest, E.R., Hevaerts, J.F. and Title, A.M., A Flu-tube tectonics model for solar coronal heating driven b the magnetic carpet, Astrophs. J. 576, 5 55 (). Priest, E.R., Hornig, G. and Pontin, D.I., On the nature of three-dimensional magnetic reconnection, J. Geophs. Res. 8, A7, SSH6- (). Schindler, K., Hesse, M. and Birn, J., General magnetic reconnection, parallel electric fields, and helicit, J. Geophs. Res. 9, A6, (988).

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

On the nature of three-dimensional magnetic reconnection

On the nature of three-dimensional magnetic reconnection JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 108, NO. A7, 1285, doi:10.1029/2002ja009812, 2003 On the nature of three-dimensional magnetic reconnection E. R. Priest School of Mathematics and Statistics, University

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

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

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

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

Coordinate geometry. + bx + c. Vertical asymptote. Sketch graphs of hyperbolas (including asymptotic behaviour) from the general

Coordinate geometry. + bx + c. Vertical asymptote. Sketch graphs of hyperbolas (including asymptotic behaviour) from the general A Sketch graphs of = a m b n c where m = or and n = or B Reciprocal graphs C Graphs of circles and ellipses D Graphs of hperbolas E Partial fractions F Sketch graphs using partial fractions Coordinate

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

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

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

10.2 The Unit Circle: Cosine and Sine

10.2 The Unit Circle: Cosine and Sine 0. The Unit Circle: Cosine and Sine 77 0. The Unit Circle: Cosine and Sine In Section 0.., we introduced circular motion and derived a formula which describes the linear velocit of an object moving on

More information

1.6 ELECTRONIC STRUCTURE OF THE HYDROGEN ATOM

1.6 ELECTRONIC STRUCTURE OF THE HYDROGEN ATOM 1.6 ELECTRONIC STRUCTURE OF THE HYDROGEN ATOM 23 How does this wave-particle dualit require us to alter our thinking about the electron? In our everda lives, we re accustomed to a deterministic world.

More information

FIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve:

FIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve: .2 INITIAL-VALUE PROBLEMS 3.2 INITIAL-VALUE PROBLEMS REVIEW MATERIAL Normal form of a DE Solution of a DE Famil of solutions INTRODUCTION We are often interested in problems in which we seek a solution

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

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

17.3. Parametric Curves. Introduction. Prerequisites. Learning Outcomes

17.3. Parametric Curves. Introduction. Prerequisites. Learning Outcomes Parametric Curves 7.3 Introduction In this Section we eamine et another wa of defining curves - the parametric description. We shall see that this is, in some was, far more useful than either the Cartesian

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

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are:

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are: Curved beams. Introduction Curved beams also called arches were invented about ears ago. he purpose was to form such a structure that would transfer loads, mainl the dead weight, to the ground b the elements

More information

16.5. Maclaurin and Taylor Series. Introduction. Prerequisites. Learning Outcomes

16.5. Maclaurin and Taylor Series. Introduction. Prerequisites. Learning Outcomes Maclaurin and Talor Series 6.5 Introduction In this Section we eamine how functions ma be epressed in terms of power series. This is an etremel useful wa of epressing a function since (as we shall see)

More information

11.4 Polar Coordinates

11.4 Polar Coordinates 11. Polar Coordinates 917 11. Polar Coordinates In Section 1.1, we introduced the Cartesian coordinates of a point in the plane as a means of assigning ordered pairs of numbers to points in the plane.

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

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 in flux-tubes undergoing spinning footpoint motions Wilmot-Smith, A. L.; De Moortel, I.

Magnetic reconnection in flux-tubes undergoing spinning footpoint motions Wilmot-Smith, A. L.; De Moortel, I. University of Dundee Magnetic reconnection in flux-tubes undergoing spinning footpoint motions Wilmot-Smith, A. L.; De Moortel, I. Published in: Astronomy and Astrophysics DOI: 10.1051/0004-6361:20077455

More information

2.5. Infinite Limits and Vertical Asymptotes. Infinite Limits

2.5. Infinite Limits and Vertical Asymptotes. Infinite Limits . Infinite Limits and Vertical Asmptotes. Infinite Limits and Vertical Asmptotes In this section we etend the concept of it to infinite its, which are not its as before, but rather an entirel new use of

More information

8 Differential Calculus 1 Introduction

8 Differential Calculus 1 Introduction 8 Differential Calculus Introduction The ideas that are the basis for calculus have been with us for a ver long time. Between 5 BC and 5 BC, Greek mathematicians were working on problems that would find

More information

8.1 Exponents and Roots

8.1 Exponents and Roots Section 8. Eponents and Roots 75 8. Eponents and Roots Before defining the net famil of functions, the eponential functions, we will need to discuss eponent notation in detail. As we shall see, eponents

More information

Methods for Advanced Mathematics (C3) Coursework Numerical Methods

Methods for Advanced Mathematics (C3) Coursework Numerical Methods Woodhouse College 0 Page Introduction... 3 Terminolog... 3 Activit... 4 Wh use numerical methods?... Change of sign... Activit... 6 Interval Bisection... 7 Decimal Search... 8 Coursework Requirements on

More information

Notes 7 Analytic Continuation

Notes 7 Analytic Continuation ECE 6382 Fall 27 David R. Jackson Notes 7 Analtic Continuation Notes are from D. R. Wilton, Dept. of ECE Analtic Continuation of Functions We define analtic continuation as the process of continuing a

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

ENGI 4430 Advanced Calculus for Engineering Faculty of Engineering and Applied Science Problem Set 3 Solutions [Multiple Integration; Lines of Force]

ENGI 4430 Advanced Calculus for Engineering Faculty of Engineering and Applied Science Problem Set 3 Solutions [Multiple Integration; Lines of Force] ENGI 44 Advanced Calculus for Engineering Facult of Engineering and Applied Science Problem Set Solutions [Multiple Integration; Lines of Force]. Evaluate D da over the triangular region D that is bounded

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

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

f x, y x 2 y 2 2x 6y 14. Then

f x, y x 2 y 2 2x 6y 14. Then SECTION 11.7 MAXIMUM AND MINIMUM VALUES 645 absolute minimum FIGURE 1 local maimum local minimum absolute maimum Look at the hills and valles in the graph of f shown in Figure 1. There are two points a,

More information

17.3. Parametric Curves. Introduction. Prerequisites. Learning Outcomes

17.3. Parametric Curves. Introduction. Prerequisites. Learning Outcomes Parametric Curves 17.3 Introduction In this section we eamine et another wa of defining curves - the parametric description. We shall see that this is, in some was, far more useful than either the Cartesian

More information

4.7. Newton s Method. Procedure for Newton s Method HISTORICAL BIOGRAPHY

4.7. Newton s Method. Procedure for Newton s Method HISTORICAL BIOGRAPHY 4. Newton s Method 99 4. Newton s Method HISTORICAL BIOGRAPHY Niels Henrik Abel (18 189) One of the basic problems of mathematics is solving equations. Using the quadratic root formula, we know how to

More information

Simultaneous Orthogonal Rotations Angle

Simultaneous Orthogonal Rotations Angle ELEKTROTEHNIŠKI VESTNIK 8(1-2): -11, 2011 ENGLISH EDITION Simultaneous Orthogonal Rotations Angle Sašo Tomažič 1, Sara Stančin 2 Facult of Electrical Engineering, Universit of Ljubljana 1 E-mail: saso.tomaic@fe.uni-lj.si

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

Green s Theorem Jeremy Orloff

Green s Theorem Jeremy Orloff Green s Theorem Jerem Orloff Line integrals and Green s theorem. Vector Fields Vector notation. In 8.4 we will mostl use the notation (v) = (a, b) for vectors. The other common notation (v) = ai + bj runs

More information

On the Extension of Goal-Oriented Error Estimation and Hierarchical Modeling to Discrete Lattice Models

On the Extension of Goal-Oriented Error Estimation and Hierarchical Modeling to Discrete Lattice Models On the Etension of Goal-Oriented Error Estimation and Hierarchical Modeling to Discrete Lattice Models J. T. Oden, S. Prudhomme, and P. Bauman Institute for Computational Engineering and Sciences The Universit

More information

Chapter Nine Chapter Nine

Chapter Nine Chapter Nine Chapter Nine Chapter Nine 6 CHAPTER NINE ConcepTests for Section 9.. Table 9. shows values of f(, ). Does f appear to be an increasing or decreasing function of? Of? Table 9. 0 0 0 7 7 68 60 0 80 77 73

More information

3.7 InveRSe FUnCTIOnS

3.7 InveRSe FUnCTIOnS CHAPTER functions learning ObjeCTIveS In this section, ou will: Verif inverse functions. Determine the domain and range of an inverse function, and restrict the domain of a function to make it one-to-one.

More information

UNCORRECTED SAMPLE PAGES. 3Quadratics. Chapter 3. Objectives

UNCORRECTED SAMPLE PAGES. 3Quadratics. Chapter 3. Objectives Chapter 3 3Quadratics Objectives To recognise and sketch the graphs of quadratic polnomials. To find the ke features of the graph of a quadratic polnomial: ais intercepts, turning point and ais of smmetr.

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

Cubic and quartic functions

Cubic and quartic functions 3 Cubic and quartic functions 3A Epanding 3B Long division of polnomials 3C Polnomial values 3D The remainder and factor theorems 3E Factorising polnomials 3F Sum and difference of two cubes 3G Solving

More information

Functions and Graphs TERMINOLOGY

Functions and Graphs TERMINOLOGY 5 Functions and Graphs TERMINOLOGY Arc of a curve: Part or a section of a curve between two points Asmptote: A line towards which a curve approaches but never touches Cartesian coordinates: Named after

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

4Cubic. polynomials UNCORRECTED PAGE PROOFS

4Cubic. polynomials UNCORRECTED PAGE PROOFS 4Cubic polnomials 4.1 Kick off with CAS 4. Polnomials 4.3 The remainder and factor theorems 4.4 Graphs of cubic polnomials 4.5 Equations of cubic polnomials 4.6 Cubic models and applications 4.7 Review

More information

What can test particles tell us about magnetic reconnection in the solar corona?

What can test particles tell us about magnetic reconnection in the solar corona? What can test particles tell us about magnetic reconnection in the solar corona? James Threlfall, T. Neukirch, C. E. Parnell, A. W. Hood jwt9@st-andrews.ac.uk @JamesWThrelfall Overview Motivation (solar

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

INTRODUCTION TO DIFFERENTIAL EQUATIONS

INTRODUCTION TO DIFFERENTIAL EQUATIONS INTRODUCTION TO DIFFERENTIAL EQUATIONS. Definitions and Terminolog. Initial-Value Problems.3 Differential Equations as Mathematical Models CHAPTER IN REVIEW The words differential and equations certainl

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

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS

KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Chapter 8 KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Figure 8.1: 195 196 CHAPTER 8. KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS 8.1 Motivation In Chapter 3, the conservation of linear momentum for a

More information

Space frames. b) R z φ z. R x. Figure 1 Sign convention: a) Displacements; b) Reactions

Space frames. b) R z φ z. R x. Figure 1 Sign convention: a) Displacements; b) Reactions Lecture notes: Structural Analsis II Space frames I. asic concepts. The design of a building is generall accomplished b considering the structure as an assemblage of planar frames, each of which is designed

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

ES.182A Topic 36 Notes Jeremy Orloff

ES.182A Topic 36 Notes Jeremy Orloff ES.82A Topic 36 Notes Jerem Orloff 36 Vector fields and line integrals in the plane 36. Vector analsis We now will begin our stud of the part of 8.2 called vector analsis. This is the stud of vector fields

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

Ordinary Differential Equations

Ordinary Differential Equations 58229_CH0_00_03.indd Page 6/6/6 2:48 PM F-007 /202/JB0027/work/indd & Bartlett Learning LLC, an Ascend Learning Compan.. PART Ordinar Differential Equations. Introduction to Differential Equations 2. First-Order

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

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

MA123, Chapter 8: Idea of the Integral (pp , Gootman)

MA123, Chapter 8: Idea of the Integral (pp , Gootman) MA13, Chapter 8: Idea of the Integral (pp. 155-187, Gootman) Chapter Goals: Understand the relationship between the area under a curve and the definite integral. Understand the relationship between velocit

More information

(MTH5109) GEOMETRY II: KNOTS AND SURFACES LECTURE NOTES. 1. Introduction to Curves and Surfaces

(MTH5109) GEOMETRY II: KNOTS AND SURFACES LECTURE NOTES. 1. Introduction to Curves and Surfaces (MTH509) GEOMETRY II: KNOTS AND SURFACES LECTURE NOTES DR. ARICK SHAO. Introduction to Curves and Surfaces In this module, we are interested in studing the geometr of objects. According to our favourite

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

Finding Limits Graphically and Numerically. An Introduction to Limits

Finding Limits Graphically and Numerically. An Introduction to Limits 8 CHAPTER Limits and Their Properties Section Finding Limits Graphicall and Numericall Estimate a it using a numerical or graphical approach Learn different was that a it can fail to eist Stud and use

More information

Conservation Laws in Ideal MHD

Conservation Laws in Ideal MHD Conservation Laws in Ideal MHD Nick Murphy Harvard-Smithsonian Center for Astrophysics Astronomy 253: Plasma Astrophysics February 3, 2016 These lecture notes are largely based on Plasma Physics for Astrophysics

More information

Vectors Primer. M.C. Simani. July 7, 2007

Vectors Primer. M.C. Simani. July 7, 2007 Vectors Primer M.. Simani Jul 7, 2007 This note gives a short introduction to the concept of vector and summarizes the basic properties of vectors. Reference textbook: Universit Phsics, Young and Freedman,

More information

Derivatives of Multivariable Functions

Derivatives of Multivariable Functions Chapter 0 Derivatives of Multivariable Functions 0. Limits Motivating Questions In this section, we strive to understand the ideas generated b the following important questions: What do we mean b the limit

More information

LESSON #42 - INVERSES OF FUNCTIONS AND FUNCTION NOTATION PART 2 COMMON CORE ALGEBRA II

LESSON #42 - INVERSES OF FUNCTIONS AND FUNCTION NOTATION PART 2 COMMON CORE ALGEBRA II LESSON #4 - INVERSES OF FUNCTIONS AND FUNCTION NOTATION PART COMMON CORE ALGEBRA II You will recall from unit 1 that in order to find the inverse of a function, ou must switch and and solve for. Also,

More information

v t t t t a t v t d dt t t t t t 23.61

v t t t t a t v t d dt t t t t t 23.61 SECTION 4. MAXIMUM AND MINIMUM VALUES 285 The values of f at the endpoints are f 0 0 and f 2 2 6.28 Comparing these four numbers and using the Closed Interval Method, we see that the absolute minimum value

More information

Differentiation and applications

Differentiation and applications FS O PA G E PR O U N C O R R EC TE D Differentiation and applications. Kick off with CAS. Limits, continuit and differentiabilit. Derivatives of power functions.4 C oordinate geometr applications of differentiation.5

More information

Introduction to Differential Equations

Introduction to Differential Equations Introduction to Differential Equations. Definitions and Terminolog.2 Initial-Value Problems.3 Differential Equations as Mathematical Models Chapter in Review The words differential and equations certainl

More information

D u f f x h f y k. Applying this theorem a second time, we have. f xx h f yx k h f xy h f yy k k. f xx h 2 2 f xy hk f yy k 2

D u f f x h f y k. Applying this theorem a second time, we have. f xx h f yx k h f xy h f yy k k. f xx h 2 2 f xy hk f yy k 2 93 CHAPTER 4 PARTIAL DERIVATIVES We close this section b giving a proof of the first part of the Second Derivatives Test. Part (b) has a similar proof. PROOF OF THEOREM 3, PART (A) We compute the second-order

More information

CH. 1 FUNDAMENTAL PRINCIPLES OF MECHANICS

CH. 1 FUNDAMENTAL PRINCIPLES OF MECHANICS 446.201 (Solid echanics) Professor Youn, eng Dong CH. 1 FUNDENTL PRINCIPLES OF ECHNICS Ch. 1 Fundamental Principles of echanics 1 / 14 446.201 (Solid echanics) Professor Youn, eng Dong 1.2 Generalied Procedure

More information

10. The dimensional formula for c) 6% d) 7%

10. The dimensional formula for c) 6% d) 7% UNIT. One of the combinations from the fundamental phsical constants is hc G. The unit of this epression is a) kg b) m 3 c) s - d) m. If the error in the measurement of radius is %, then the error in the

More information

8. BOOLEAN ALGEBRAS x x

8. BOOLEAN ALGEBRAS x x 8. BOOLEAN ALGEBRAS 8.1. Definition of a Boolean Algebra There are man sstems of interest to computing scientists that have a common underling structure. It makes sense to describe such a mathematical

More information

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x 5A galler of graphs Objectives To recognise the rules of a number of common algebraic relations: = = = (rectangular hperbola) + = (circle). To be able to sketch the graphs of these relations. To be able

More information

VECTORS IN THREE DIMENSIONS

VECTORS IN THREE DIMENSIONS 1 CHAPTER 2. BASIC TRIGONOMETRY 1 INSTITIÚID TEICNEOLAÍOCHTA CHEATHARLACH INSTITUTE OF TECHNOLOGY CARLOW VECTORS IN THREE DIMENSIONS 1 Vectors in Two Dimensions A vector is an object which has magnitude

More information

Mathematics Extension 2

Mathematics Extension 2 Student Number ABBOTSLEIGH AUGUST 007 YEAR ASSESSMENT 4 HIGHER SCHOOL CERTIFICATE TRIAL EXAMINATION Mathematics Etension General Instructions Reading time 5 minutes. Working time 3 hours. Write using blue

More information

Lab 5 Forces Part 1. Physics 211 Lab. You will be using Newton s 2 nd Law to help you examine the nature of these forces.

Lab 5 Forces Part 1. Physics 211 Lab. You will be using Newton s 2 nd Law to help you examine the nature of these forces. b Lab 5 Forces Part 1 Phsics 211 Lab Introduction This is the first week of a two part lab that deals with forces and related concepts. A force is a push or a pull on an object that can be caused b a variet

More information

10.5 Graphs of the Trigonometric Functions

10.5 Graphs of the Trigonometric Functions 790 Foundations of Trigonometr 0.5 Graphs of the Trigonometric Functions In this section, we return to our discussion of the circular (trigonometric functions as functions of real numbers and pick up where

More information

STUDY KNOWHOW PROGRAM STUDY AND LEARNING CENTRE. Functions & Graphs

STUDY KNOWHOW PROGRAM STUDY AND LEARNING CENTRE. Functions & Graphs STUDY KNOWHOW PROGRAM STUDY AND LEARNING CENTRE Functions & Graphs Contents Functions and Relations... 1 Interval Notation... 3 Graphs: Linear Functions... 5 Lines and Gradients... 7 Graphs: Quadratic

More information

Finding Limits Graphically and Numerically. An Introduction to Limits

Finding Limits Graphically and Numerically. An Introduction to Limits 60_00.qd //0 :05 PM Page 8 8 CHAPTER Limits and Their Properties Section. Finding Limits Graphicall and Numericall Estimate a it using a numerical or graphical approach. Learn different was that a it can

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

Additional Material On Recursive Sequences

Additional Material On Recursive Sequences Penn State Altoona MATH 141 Additional Material On Recursive Sequences 1. Graphical Analsis Cobweb Diagrams Consider a generic recursive sequence { an+1 = f(a n ), n = 1,, 3,..., = Given initial value.

More information

Fluid Mechanics II. Newton s second law applied to a control volume

Fluid Mechanics II. Newton s second law applied to a control volume Fluid Mechanics II Stead flow momentum equation Newton s second law applied to a control volume Fluids, either in a static or dnamic motion state, impose forces on immersed bodies and confining boundaries.

More information

APPENDIXES. B Coordinate Geometry and Lines C. D Trigonometry E F. G The Logarithm Defined as an Integral H Complex Numbers I

APPENDIXES. B Coordinate Geometry and Lines C. D Trigonometry E F. G The Logarithm Defined as an Integral H Complex Numbers I APPENDIXES A Numbers, Inequalities, and Absolute Values B Coordinate Geometr and Lines C Graphs of Second-Degree Equations D Trigonometr E F Sigma Notation Proofs of Theorems G The Logarithm Defined as

More information

2.2 SEPARABLE VARIABLES

2.2 SEPARABLE VARIABLES 44 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 6 Consider the autonomous DE 6 Use our ideas from Problem 5 to find intervals on the -ais for which solution curves are concave up and intervals for which

More information

11.1 Double Riemann Sums and Double Integrals over Rectangles

11.1 Double Riemann Sums and Double Integrals over Rectangles Chapter 11 Multiple Integrals 11.1 ouble Riemann Sums and ouble Integrals over Rectangles Motivating Questions In this section, we strive to understand the ideas generated b the following important questions:

More information

Numerical Simulations of 3D Reconnection: rotating footpoints

Numerical Simulations of 3D Reconnection: rotating footpoints Numerical Simulations of 3D Reconnection: rotating footpoints I. De Moortel 1, K. Galsgaard 2 1 University of St Andrews, UK 2 Niels Bohr Institute, Denmark Contents: - numerical setup - description of

More information

ZETA MATHS. Higher Mathematics Revision Checklist

ZETA MATHS. Higher Mathematics Revision Checklist ZETA MATHS Higher Mathematics Revision Checklist Contents: Epressions & Functions Page Logarithmic & Eponential Functions Addition Formulae. 3 Wave Function.... 4 Graphs of Functions. 5 Sets of Functions

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

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

Pure Further Mathematics 2. Revision Notes

Pure Further Mathematics 2. Revision Notes Pure Further Mathematics Revision Notes October 016 FP OCT 016 SDB Further Pure 1 Inequalities... 3 Algebraic solutions... 3 Graphical solutions... 4 Series Method of Differences... 5 3 Comple Numbers...

More information

18.02 Review Jeremy Orloff. 1 Review of multivariable calculus (18.02) constructs

18.02 Review Jeremy Orloff. 1 Review of multivariable calculus (18.02) constructs 18.02 eview Jerem Orloff 1 eview of multivariable calculus (18.02) constructs 1.1 Introduction These notes are a terse summar of what we ll need from multivariable calculus. If, after reading these, some

More information

Section 1.2: A Catalog of Functions

Section 1.2: A Catalog of Functions Section 1.: A Catalog of Functions As we discussed in the last section, in the sciences, we often tr to find an equation which models some given phenomenon in the real world - for eample, temperature as

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

Applications of Derivatives

Applications of Derivatives 58_Ch04_pp86-60.qd /3/06 :35 PM Page 86 Chapter 4 Applications of Derivatives A n automobile s gas mileage is a function of man variables, including road surface, tire tpe, velocit, fuel octane rating,

More information

Analytic Geometry in Three Dimensions

Analytic Geometry in Three Dimensions Analtic Geometr in Three Dimensions. The Three-Dimensional Coordinate Sstem. Vectors in Space. The Cross Product of Two Vectors. Lines and Planes in Space The three-dimensional coordinate sstem is used

More information

NST1A: Mathematics II (Course A) End of Course Summary, Lent 2011

NST1A: Mathematics II (Course A) End of Course Summary, Lent 2011 General notes Proofs NT1A: Mathematics II (Course A) End of Course ummar, Lent 011 tuart Dalziel (011) s.dalziel@damtp.cam.ac.uk This course is not about proofs, but rather about using different techniques.

More information

Astronomy. Astrophysics. Numerical modelling of 3D reconnection. II. Comparison between rotational and spinning footpoint motions

Astronomy. Astrophysics. Numerical modelling of 3D reconnection. II. Comparison between rotational and spinning footpoint motions A&A 459, 627 639 (2006) DOI: 10.1051/0004-6361:20065716 c ESO 2006 Astronomy & Astrophysics Numerical modelling of 3D reconnection II. Comparison between rotational and spinning footpoint motions I. De

More information

Closed form expressions for the gravitational inner multipole moments of homogeneous elementary solids

Closed form expressions for the gravitational inner multipole moments of homogeneous elementary solids Closed form epressions for the gravitational inner multipole moments of homogeneous elementar solids Julian Stirling 1,2, and Stephan Schlamminger 1 1 National Institute of Standards and Technolog, 1 Bureau

More information