The Harris-sheet model provides an elegant solution to the kinetic plasma equation for a steady state 1D current sheet geometry separating regions with oppositely directed magnetic field. However, adding just a small normal magnetic field to the Harris configuration yields thermal streaming of particles into and out of the current sheet, fundamentally changing the form of its kinetic description. The action variable, J z, associated with the oscillatory orbit motion perpendicular to the current sheet is well conserved and can be applied for solving the kinetic equation in the 1D sheet geometry that includes a small normal magnetic field. Revisiting this problem, we develop a new formalism that permits numerical solutions to be readily obtained for general upstream/asymptotic electron and ion distributions. In particular, we consider the case of isotropic ion pressure and anisotropic bi-Maxwellian electrons. The current sheets are then supported by electron pressure anisotropy. Furthermore, the total current across a particular sheet is set by the fire-hose condition based on the electron pressures normalized by the asymptotic magnetic field pressure. Analytical approximations are obtained for the numerical solutions expressed in terms of the asymptotic electron temperature anisotropy and the ion temperature. We discuss a preliminary application of the framework to the electron diffusion region of anti-parallel magnetic reconnection.

Plasma current sheets have been observed in nearly all regions of space accessed in situ by spacecraft. For example, the ongoing Parker Solar Probe mission has recently provided direct observations of the heliopsheric current sheet at locations less than 0.2 AU from the Sun,1 while the current sheet of the Earth's magnetotail was encountered by the early Imp 1 mission.2 Even before the first space observations, current sheets were diagnosed in laboratory pinch experiments3 and motivated Dr. Harris to report on the now-renowned Harris model for 1D current sheets.4 

The Harris sheet configuration has served as the starting point for countless theoretical and numerical investigations, including modern spacecraft observations,5 current sheet stability,6 and magnetic reconnection.7 It provides an exact closed-form analytical solution to the full Vlasov–Maxwell system of equations, constituting a kinetic description of a 1D plasma current sheet separating oppositely directed magnetic fields. As an illustration of the geometry, the Harris profiles of the current density and magnetic field are shown in Figs. 1(a) and 1(b) corresponding to the analytical solutions,
J ( z ) = B 0 μ 0 δ sech 2 ( z δ ) e y ,
(1)
B ( z ) = B 0 tanh ( z δ ) e x .
(2)
Here, B0 is the asymptotic magnetic field strength that reverses its direction across the sheet, μ0 is the vacuum permeability, and sech ( x ) = 1 / cosh ( x ). The thickness of the sheet is set by δ.
FIG. 1.

(a) and (b) Illustration of the Harris sheet current density and magnetic field given in Eqs. (1) and (2), respectively. (c)–(e) Electron orbit in a Harris sheet geometry augmented with small normal magnetic field component, B z = B 0 / 10. The energy of the electron is E δ = ( e δ B 0 ) 2 / ( 2 m e ).

FIG. 1.

(a) and (b) Illustration of the Harris sheet current density and magnetic field given in Eqs. (1) and (2), respectively. (c)–(e) Electron orbit in a Harris sheet geometry augmented with small normal magnetic field component, B z = B 0 / 10. The energy of the electron is E δ = ( e δ B 0 ) 2 / ( 2 m e ).

Close modal
To approximate certain naturally occurring systems (like the Earth's magnetotail8), it can be important to include a normal magnetic field, Bz. Here, the normal magnetic field has been associated with double peaked current sheets, and its presence strongly influences the onset of magnetic reconnection.9–13 The strong impact of a finite Bz is perhaps not surprising as it changes fundamental properties of the system. For example, when imposing a non-zero Bz onto the Harris solution, an unbalance force appears in the x-direction, F x = J y B z, violating the equilibrium condition. In fact, earlier work14–16 show that 1D current layers (including a normal magnetic field) can only be in equilibrium if the asymptotic plasma has an anisotropic pressure characterized by the marginal fire-hose condition,
B 0 2 μ 0 = P | | 0 P 0 .
(3)
Here, respectively, P | | 0 and P 0 are the total asymptotic plasma pressure components parallel and perpendicular to the asymptotic magnetic field.

Another complication to the Harris solution is evident in Fig. 1(c), where the black lines represent projections of the magnetic field lines onto the xz-plane. A typical trajectory of a thermal electron is illustrated by the blue line. Due to the finite Bz component, the electrons stream along the magnetic field into the center of the current sheet, where they reflect and are again ejected. This type of trajectory is known as a Speiser orbit,17 with other projections shown in Figs. 1(d) and 1(e). Irrespective of how small | B z | may be, any finite value of Bz will result in the described free streaming of particles across the sheet, not respected by the Harris solution.

Given the rapid z-oscillations of the Speiser orbit, the associated action integral J z v z d z is an adiabatic invariant,18,19 provided that the normal magnetic field is small.20 This current sheet invariant has been explored for solving the kinetic equation of the 1D current sheet problem, by writing the phase-space distributions in the form
f σ ( z , v ) = f σ 0 ( U , J z ) , U = m e v 2 2 + q σ Φ ( z ) .
(4)
Here, U is the total particle energy, Φ ( z ) is the electrostatic potential, f σ 0 is the asymptotic phase-space distribution, while q σ is the charge for particle species σ. In the present paper, we will also study solutions provided by Eq. (4); these results are complementary and generally in agreement with earlier work21–23 on this problem.

The paper is organized as follows: For fixed profiles of B x ( z ) and Φ ( z ), in Sec. II, we discuss in more detail the current sheet adiabatic invariant, J z, as well as our general approach for obtaining solutions to Eq. (4). In Sec. III, a numerical scheme is detailed by which self-consistent profiles of B x ( z ) and Φ ( z ) are determined and analytical approximations for these profiles are derived. Relevant to kinetic simulations of reconnection, Sec. IV includes an analysis of modifications to the numerical solutions caused by non-monotonic electrostatic Φ ( z )-profiles. The paper is concluded in Sec. V.

The present type of kinetic problem involving free streaming of particles along some variable magnetic field can in many cases be solved using the drift-kinetic framework.24 For example, for the considered 1D geometry, within the regions where the magnetic moment μ = m v 2 / ( 2 B ) is an adiabatic invariant, a steady state drift-kinetic solution to the free-streaming particles can in certain cases be written as f σ = f σ 0 ( U , μ ). However, a solution of this form is not applicable to the center of a current sheet where μ breaks as an adiabatic invariant.

To elucidate the dynamics that lead to the breakdown of μ, we recall that its invariance is directly tied to its properties as an action integral. In terms of the gyrophase ϕ and the Larmor radius ρ L = m v / ( e B ), this action integral takes the form
μ = e 4 π 0 2 π v ρ L d ϕ = e 4 π v y d y + e 4 π v z d z .
(5)
Away from z 0, the particles execute their regular cyclotron orbits with well-conserved values of μ. In this outside region, the vy and vz contributions on the right of Eq. (5) are identical. The breakdown of μ occurs abruptly as the electrons transition into the Speiser orbits. For the sections of meandering orbit motion across the current layer, vy does not change sign and there is no periodic motion in the y-direction. Therefore, the v y d y-integral in Eq. (5) cannot be computed, and μ is undefined.
Meanwhile, the situation is different for the dynamics in the z-direction, as it is evident from Figs. 1(c) and 1(d) that orbits in the current layer geometry include well-defined z-oscillations. The action integral v z d z is an adiabatic invariant,19,20 but it should be noted that the transition from the regular cyclotron motion into the meandering motion can be understood as a merger at z = 0 between two cyclotron orbits. Thus, during this merger, the v z d z-integral doubles.20 Based on this observation, we normalize this J z-action by the expression
J z { e 2 π v z d z , cyclotron , e 4 π v z d z , meandering .
(6)
With this definition, J z remains a good adiabatic invariant as the particles pass in and out of the current sheet. This also relies on our assumption of only including a small normal magnetic field, such that the typical Larmor radius of the particles ρL is much larger than the radius of curvature Rc of the magnetic field for z = 0. The curvature parameter κ = R c / ρ L 1 is then small and characterizes the quasi-adiabatic regime where the change in J z as a particle travels in and out of current sheet is on the order of κ J z.20 Furthermore, with our choice for normalization in Eq. (6), it also follows that in the external regions (where v y d y = v z d z), we simply have J z = μ.
For given profiles of B x ( z ) and Φ ( z ), we develop methods by which J z is efficiently evaluated as a function of ( z , v y , v z ). Because of the invariance of J z, the solution in Eq. (4) is valid across the current sheet. In turn, a numerical search allows the self-consistent profiles of B x ( z ) and Φ ( z ) to be determined, which honor both Ampère's law, μ 0 J y ( z ) = B x / z, and the condition of quasi-neutrality, n i ( z ) = n e ( z ). While not imposed directly, the obtained solutions are also consistent with the force balance constraint along the current sheet in Eq. (3), as well as perpendicular to the sheet where
B x 2 ( z ) 2 μ 0 + P x x ( z ) = constant .
(7)
The outlined approach is similar to the drift-kinetic model24 but includes some important differences. Contrary to the drift-kinetic approach where μ = m e v 2 / ( 2 B ) is only the first term in an expansion of the full adiabatic invariant,25 here we will evaluate J z ( z , v y , v z ) without any approximation. As a result, Eq. (4) provides a steady state solution to the full kinetic equation [ f σ / t + x · v f σ + ( q / m ) v · ( E + v × B ) f σ = 0].

While our approach is general, we limit our investigations to the case where the ions are characterized by isotropic pressure with an uniform temperature Ti across the geometry. Meanwhile, the electrons are allowed to be anisotropic, characterized by asymptotic temperatures T e | | 0 and T e 0, parallel and perpendicular to the asymptotic magnetic field, respectively. In the asymptotic plasma, the electrons and ions share the common number density n0.

To aid the analysis, we introduce the following quantities useful for normalizing physical parameters:
E δ = T e | | 0 T e 0 ,
(8)
B 0 = μ 0 n 0 ( T e | | 0 T e 0 ) ,
(9)
δ = 2 m e E δ e B 0 ,
(10)
J 0 = B 0 μ 0 δ , J z 0 = E δ B 0 .
(11)
For the case in Fig. 1, where we simply explored an electron orbit, B0 and δ represent the free parameters in the Harris sheet solution. A characteristic electron energy related to the width of the current layer may here be defined as E δ = ( e B 0 δ ) 2 / ( 2 m e ). Meanwhile, later it will become clear that the fields of the self-consistent solutions for a particular set of the asymptotic temperatures can be approximated through the Harris profiles in Eqs. (1) and (2) when using E δ in Eq. (8) in combination with the expressions for B0 and δ in Eqs. (9) and (10), respectively. Characteristic values of the current density and the J z-action variable are defined in Eq. (11).

The field-reverse-configuration (FRC) considered for magnetic confinement of fusion plasma26 turns out to have orbit dynamics very similar to the 1D current sheets considered here. As such, the analysis below for electrons in the 1D current sheet closely follows the approach developed in Ref. 27 for analyzing the fast ion behavior in the FRC. For the present analysis, we choose coordinates such that the infinite current sheet J ( z ) e y flows in the y-direction and is symmetrical about z = 0 such that J ( z ) = J ( z ). Again, the geometry is illustrated in Fig. 1(a), which by Ampère's law yields the magnetic field reversal in the asymptotic magnetic field B0 in the x-direction illustrated in Fig. 1(b). Throughout the analysis, we include a normal magnetic field such that B = [ B x ( z ) , 0 , B z ]. It is assumed that | B z | is small, and while the final results of the analysis turn out to be independent of Bz, all illustrations are obtained with B z = B 0 / 10.

In our analysis, we also include a finite electric field, Ez. Initially, we focus on the case where Ez is directed toward z = 0, illustrated in Fig. 2(a). Thus, the electrostatic potential, Φ = 0 z E z d z , has the form shown in Fig. 2(b), symmetric about z = 0 with a single global minimum for z = 0. As will be discussed later, the profiles in Fig. 2 are self-consistently obtained for an upstream bi-Maxwellian electron distribution with T e 0 / T e 0 = 4, and with isotropic ions characterized by T i = T e | | 0.

FIG. 2.

(a) and (b) Example profiles of Ez and Φ considered in the preliminary analysis. (c) and (d) Effective potential Φ eff defined in Eq. (15), evaluated as a function of z for x T / δ = 20 and x T / δ = 7, respectively. (e) Color contours of Φ eff as a function of ( x T , z ). (f) Color contours of vz as defined in Eq. (17), as a function of z and xT for z T / δ = 3.5. (g) Color contours of the J z action variable as a function of (xT, zT). The white lines highlight a particular contour level of J z, which characterizes turning points of the red trajectory.

FIG. 2.

(a) and (b) Example profiles of Ez and Φ considered in the preliminary analysis. (c) and (d) Effective potential Φ eff defined in Eq. (15), evaluated as a function of z for x T / δ = 20 and x T / δ = 7, respectively. (e) Color contours of Φ eff as a function of ( x T , z ). (f) Color contours of vz as defined in Eq. (17), as a function of z and xT for z T / δ = 3.5. (g) Color contours of the J z action variable as a function of (xT, zT). The white lines highlight a particular contour level of J z, which characterizes turning points of the red trajectory.

Close modal
The 1D magnetic configuration (with By = 0) is fully described by the Ay-component of the magnetic vector potential,
A y ( x , z ) = x B z 0 z B x ( z ) d z ,
(12)
where contours of A y = constant coincide with the magnetic field lines. The Lagrangian for the electron motion is L ( x , z ) = e v y A y ( x , z ) + m e v 2 / 2 + e Φ ( z ), which is observed to be independent of y. Given this symmetry in the y-direction, the canonical momentum,
p y ( x , z , v y ) = L v y = e A y + m e v y ,
(13)
is a constant of motion simply because p y / t = L / y = 0.
For any initial condition ( x 0 , z 0 , v y 0 ), we can evaluate the corresponding canonical momentum p y 0 = p y ( x 0 , z 0 , v y 0 ). Information about vy as a function of (x, z) can then be obtained by analyzing p y ( x , z , v y ) = p y 0. Meanwhile, we notice that x only appears in the expression for py through the linear term xBz in Eq. (12), and we can therefore always pick a coordinate system where p y 0 = 0. To be more specific, with x T = x p y 0 / ( e B z ), the constraint p y ( x , z , v y ) = p y 0 can be expressed as
e A y ( x T , z ) + m e v y = 0 .
(14)
Physically, with this choice for xT, the corresponding electron is “tied” to the magnetic field line that passes through ( x T , z ) = ( 0 , 0 ). To illustrate this property, the orbit shown in Fig. 1(c) was computed with p y 0 = 0, such that x = xT.
Using the adiabatic framework, it is assumed for the purpose of calculating J z that the electrons bounce rapidly in the z-direction, such that this motion can be evaluated at a fixed xT and a fixed total perpendicular energy given by
U y z = m e ( v y 2 + v z 2 ) / 2 e Φ ( z ) = m e v z 2 / 2 + e Φ eff .
(15)
Here, we have introduced the effective potential e Φ eff m e v y 2 / 2 e Φ ( z ), which through the use of Eq. (14) for any fixed xT only depends on z,
Φ eff ( z ; x T ) = ( e A y ( x T , z ) ) 2 2 e m e Φ ( z ) .
(16)
Profiles of Φ eff ( z ; x T ) have two distinct types, depending on the value of xT. The profile in Fig. 2(c) is evaluated for x T / δ = 20 and displays a local maximum of Φ eff for z = 0. Corresponding to the regular cyclotron motion around the A y ( x T , z ) = 0 field line, electrons with Uyz below the local maximum of Φ eff will be trapped in one of the local wells. In contrast, electrons with larger Uyz are characterized by meandering orbits across the current sheet. In Fig. 2(d), we show Φ eff ( z ) evaluated for x T / δ = 7, where the profile includes a single global minimum at z = 0. Generally, for positive values of xT, all electron orbits are of the meandering type.

The color contours in Fig. 2(e) illustrate Φ eff as a function of ( x T , z ). The cyan line is again the field line characterized by A y ( x T , z ) = 0, and the cuts considered in panels (c) and (d) are marked by the black dashed lines. The transition points identified in panel (c) fall on the magenta line, marking the bifurcation between cyclotron and meandering orbits. As such, the line encloses the regions of local cyclotron motion; any electron bouncing to the left of the magenta line performs regular cyclotron motion, whereas electrons that reach regions to the right of the line follow the meandering motion.

For a given electron orbit bouncing in z at a fixed xT, let zT represent the turning points where vz = 0. The bounce motion perpendicular to the x-direction is then fully parameterized by (xT, zT), as the perpendicular energy in Eq. (15) is then known U y z = e Φ eff ( x T , z T ). In turn, for given values of (xT, zT), we may also compute vz as a function of z,
v z ( z ) = 2 e m e [ Φ eff ( x T , z T ) Φ eff ( x T , z ) ] .
(17)
In Fig. 2(f), a particular choice is marked for zT, and the color contours represent vz evaluated as a function of ( x T , z ).

With Eq. (17), profiles like the one in Fig. 2(f) are readily evaluated for any zT, and all information required for computing J z in Eq. (6) can therefore be obtained as a function of z for any set of (xT, zT). As an example, in Fig. 2(g), the color contours of constant J z are presented in the (xT, zT)-plane. The white lines highlight a particular contour level of J z corresponding to the orbit shown by the red line. It is evident that J z is well conserved for this orbit as all of the orbit bounce points consistently fall on the white lines. We notice from Fig. 2(e) that Φ eff increases with the distance away from the Ay = 0 contour such that arbitrary large values of Uyz can be accommodated by considering a sufficiently large domain size.

For the considered type of current sheets, J z is readily computed as a function of (xT, zT). Meanwhile, for evaluating the solution in Eq. (4), it is desirable to cast J z as a function of ( z , v y , v z ). Here, from Eq. (12), it is clear that A y ( x T , z ) = A y ( 0 , z ) + x T B z, and using this in Eq. (14), it then follows
x T = e A y ( 0 , z ) + m e v y e B z .
(18)
Next, values of zT can be determined as the roots of
e Φ eff ( x T , z T ) = e Φ eff ( x T , z ) + 1 2 m e v z 2 .
(19)
This then allows both xT and zT to be evaluated as a function of ( z , v y , v z ). Based on these results and observations, we have implemented in MATLAB numerical routines that as a function of ( z , v y , v z ) first solve for (xT, zT) using Eqs. (18) and (19). In turn, J z ( z , v y , v z ) is then readily evaluated through interpolation in the type of J z ( x T , z T )-map shown in Fig. 2(g).

Our analysis centers on the previous and well-established result that J z is conserved for particles entering and exiting the current sheet. Using the methods developed above for evaluating J z ( z , v y , v z ), solutions for the electron distribution, f ( z , v ) (where for convenience, we have dropped subscript e) of the form in Eq. (4) are then readily obtained for specified profiles of B(z) and Φ ( z ).

To further elucidate the approach, in Figs. 3(a)–3(c), color contours of constant J z are shown as a function of (vy, vz) for z / δ { 7 , 2 , 0 }. Here, the thermal electrons at z = 7 δ are sufficiently far away from the current sheet that they are characterized by the regular perpendicular cyclotron motion. Consequently, in Figs. 3(a), the contours of constant J z are concentric circles centered on ( v y , v z ) = ( 0 , 0 ). This result is characteristic for locations outside the current sheet where, as discussed above, J z = μ. For z = 2 δ considered in Fig. 3(b), electrons with v y / v 0 1 are influenced by the proximity of the current sheet yielding reduced values of J z. This effect is more noticeable at the center of the current sheet (z = 0) for which values of J z in Fig. 3(c) are reduced significantly for v y < 0. Consistent with the trajectory shown in Figs. 1(c)–1(e), at the center of the current sheet, large speeds in the negative y-direction will be deflected by the small Bz into the negative x-direction. Thus, for meandering orbits (all characterized by v y < 0), a reduced fraction of vy is available to be deflected into the z-direction during the orbit motion. As a consequence, the values of J z are reduced compared to orbits with similar negative values of vy outside the current sheet.

FIG. 3.

(a)–(c) Color contours of log 10 ( J z / J z 0 ) as a function of (vy, vz) for z / δ { 7 , 2 , 0 }. (d)–(f) Solutions for f ( z , v ) obtained from Eq. (4) using an f0 with T e | | 0 / T e 0 = 4. Color contours of log 10 [ f / f 0 ( v = 0 ) ] at vx = 0 as a function of (vy, vz) for z / δ { 7 , 2 , 0 }.

FIG. 3.

(a)–(c) Color contours of log 10 ( J z / J z 0 ) as a function of (vy, vz) for z / δ { 7 , 2 , 0 }. (d)–(f) Solutions for f ( z , v ) obtained from Eq. (4) using an f0 with T e | | 0 / T e 0 = 4. Color contours of log 10 [ f / f 0 ( v = 0 ) ] at vx = 0 as a function of (vy, vz) for z / δ { 7 , 2 , 0 }.

Close modal

For the cases where the asymptotic distribution is isotropic, f 0 ( U , J z ) = f 0 ( U ), the full solution f ( z , v ) = f 0 ( U , J z ) remains isotropic for any z independent of J z, and will carry zero current. To search for meaningful solutions consistent with a finite current density of the reversing magnetic field, it is required that f0 be anisotropic. We therefore explore solutions to Eq. (4) where f0 is a bi-Maxwellian characterized by T e | | 0 > T e 0.

Corresponding to the profiles of J z in Figs. 3(a)–3(c) and an f0 with T e | | 0 / T e 0 = 4, in Figs. 3(d)–3(f), contours of constant f ( z , v ) are evaluated for vx = 0 and z / δ { 7 , 2 , 0 }. Note that for the present choice of f0, from Eq. (4), it follows that
f ( z , v ) = f ( z , v y , v z ) | v x = 0 exp ( m e v x 2 2 T e | | 0 ) ,
such that the full distributions can be deduced from the contours in Figs. 3(d)–3(f). Outside the current sheet for z / δ = 7 in panel (d), the distribution is characterized by the asymptotic form, f0. In contrast, for z / δ = 2 in panel (e), the region of reduced J z for v y < 0 yields enhanced values of f. This effect is most pronounced for the center of the current sheet shown in panel (f).

We first discuss how the self-consistent profiles of B x ( z ) can be determined for T i T e 0. For this case, the ions respond very strongly to Φ ( z ), and quasi-neutrality then requires that e Φ T i T e 0, such that Φ = 0 is a good approximation when solving for the electron distributions.

The described enhanced levels of f in Figs. 3(e) and 3(f) for v y < 0 yield a net electron current in the y-direction, and we apply an iterative scheme to determine the self-consistent profile of B x ( z ) that matches the current profiles carried by these electrons. At iteration step k, for a given f0 and profile of B x k ( z ), we apply 200 evenly spaced values of z for which distributions f k ( z , v ) of the types in Figs. 3(d)–3(f) are computed. From these distributions, J y k ( z ) = e v y f k d 3 v is evaluated and the matching magnetic field is then readily computed B x J y k ( z ) = μ 0 0 z J y k ( z ) d z . As illustrated in Fig. 4(a), for the subsequent iterative steps, we use B x k + 1 ( z ) = [ B x k ( z ) + B x J y k ( z ) ] / 2, where the first guess of B x 1 ( z ) is shown by the black line. The solution quickly converges to reach its self-consistent form after just seven iterations. The corresponding profiles of the current density Jy and number density n are shown in Figs. 4(b) and 4(c). Here, the final profile of n displays a peak at the center of the current sheet, with an amplitude of about 150% of the asymptotic density.

FIG. 4.

(a)–(c) Normalized profiles of B x k ( z ) , J y k ( z ), and n e k ( z ). Here, k represents the step in the iteration procedure, marked by the line-colors as indicated in the panels. (d)–(f) Various profiles as a function of z obtained from moments of the fully converged solution of f. In particular, the profiles in (e) verifies the force balance constraint in Eq. (7), while the profiles in (f) demonstrate how the solutions also adhere to the marginal fire-hose condition in Eq. (3).

FIG. 4.

(a)–(c) Normalized profiles of B x k ( z ) , J y k ( z ), and n e k ( z ). Here, k represents the step in the iteration procedure, marked by the line-colors as indicated in the panels. (d)–(f) Various profiles as a function of z obtained from moments of the fully converged solution of f. In particular, the profiles in (e) verifies the force balance constraint in Eq. (7), while the profiles in (f) demonstrate how the solutions also adhere to the marginal fire-hose condition in Eq. (3).

Close modal

To test the self-consistent properties of the converged solution in Figs. 4(d)–4(f), we display various profiles related to the temperature and pressure components varying across the current sheet. Because vx and vz only appear in the model through v x 2 and v z 2 [like in Eq. (19)], the distributions are even in these. Thus, the model includes no off diagonal stress and only the elements on the diagonal of the pressure tensor are finite. As usual, these elements are defined by P eii = m e ( v i v i ) 2 f e ( v ) d 3 v, with i { x , y , z }.

The profile of T exx = P exx / n is constant, whereas T eyy = P eyy / n displays a substantial increase compared to the external value, imposed by the applied asymptotic distribution. The combination of the more modest increase in Tezz and the peaked density profile produce the profile of Pezz shown in Fig. 4(e). Consistent with force balance across the current layer, we observe that P ezz + B x 2 / ( 2 μ 0 ) is constant across the current layer (see red line marked “sum”). This illustrates how the numerical approach provides kinetic solutions that fulfill the fluid force balance in the z-direction across the current sheet.

With Eq. (3), we discussed how the marginal fire-hose condition needs to be satisfied in the asymptotic region in order for the current layer to be in overall force balance in the x-direction. In our numerical scheme, the asymptotic value of Bx is not prescribed. Rather, as shown in Fig. 4(a), during the course of the iterations, it quickly evolves toward the expected value characterized by B0 in Eq. (9). Thus, the iterative solution in Fig. 4(f) demonstrates how the profile of P e | | P e [ = P exx ( P eyy + P ezz ) / 2 ] coincides with B x 2 / μ 0 for z / δ < 2.5, and the calculation emphasizes how the pressure anisotropy in the asymptotic region is directly responsible of driving the total current across the current sheet. In fact, with K = J y d z being the total current per unit length of the layer, from Ampère's law and Eq. (3), it follows that in the case of a 1D current sheet with isotropic ions, we generally have
K = 2 P e | | 0 P e 0 / μ 0 .
(20)
For an isotropic temperature Ti, we assume that the density of the ions follows the Boltzmann scaling,
n i ( z ) = n 0 exp ( e Φ ( z ) T i ) .
(21)
Numerical routines are then applied to solve for the profile of Φ ( z ) that yields n e ( z ) = n i ( z ). Let n e k ( z ) and n i k ( z ) be the profiles obtained with Φ k ( z ), at iteration step k. For the next step, k + 1, we then use
Φ ( z ) k + 1 = Φ ( z ) k λ T i e log ( n i k ( z ) n e k ( z ) n 0 ) ,
(22)
where the choice of λ = 0.15 provides a steady and numerically robust convergence toward the solution corresponding to a particular set of T e 0 / T e 0 and T i / T e 0. Using the procedure outlined in Sec. III A, in a search, we first solve for the self-consistent profile of B x ( z ) at the considered value of T e 0 / T e 0 while imposing Φ = 0. Next, a fully converged solution including a self-consistent profile of Φ ( z ) is obtained in about 20 additional iterations where the search is augmented with Eq. (22).

Numerical solutions to the 1D current sheet problem are obtained for a matrix spanned by three separate values of T e 0 / T e 0 and three separate values of T i / T e 0. In Fig. 5, the resulting profiles are displayed, where as indicated in panel (f), the blue, green, and red lines correspond to T i / T e 0 { 0.1 , 1 , 10 }, respectively. As marked at the top of the columns, panels (a)–(f), (g)–(l), and (m)–(r) correspond to T e 0 / T e 0 { 3 / 2 , 3 , 6 }, respectively. Meanwhile, the black dashed lines are the result of curve fitting to the numerical profiles. In all cases, these approximate profiles are in good agreement with those evaluated numerically. In the following, we describe the approximate form obtained for each of the quantities.

FIG. 5.

Numerical profiles of various parameters in self-consistent current sheet configurations. As indicated at the top, the three columns of panels (a)–(f), (g)–(l), and (m)–(r) were obtained with T e | | 0 / T e 0 { 1.5 , 3 , 6 }, respectively. The legends for the line colors are given in panel in (f); blue, red, and green lines correspond to T i / T e | | 0 { 0.1 , 1 , 10 }, respectively. In many cases, the profiles are relatively insensitive to T i / T e | | 0, such that the lines have significant overlap. The black dashed lines represent the approximations described in the text.

FIG. 5.

Numerical profiles of various parameters in self-consistent current sheet configurations. As indicated at the top, the three columns of panels (a)–(f), (g)–(l), and (m)–(r) were obtained with T e | | 0 / T e 0 { 1.5 , 3 , 6 }, respectively. The legends for the line colors are given in panel in (f); blue, red, and green lines correspond to T i / T e | | 0 { 0.1 , 1 , 10 }, respectively. In many cases, the profiles are relatively insensitive to T i / T e | | 0, such that the lines have significant overlap. The black dashed lines represent the approximations described in the text.

Close modal
In all panels of Fig. 5, the z-coordinates are normalized by δ as given in Eq. (10). From panels (a), (g), and (m), however, it is clear that the width of the current layers is also weakly sensitive to T i / T | | 0 as well as T e | | 0 / T e 0 in a way not captured by Eq. (10). Through curve fitting, we obtain a more accurate approximation for the current layer width
δ * = 2 m e E δ / ( e B 0 ) 0.85 + T e 0 3 T e 0 + 0.45 ( n z = 0 n 0 1 ) ,
(23)
where E δ and B0 are defined in Eqs. (8) and (9), respectively. The term n z = 0 / n 0 represents the central density normalized by the density of the asymptotic plasma; the term can be estimated directly using the approximations that are given as follows.
The expressions for the Harris-like magnetic field and current profiles are generalized with δ * and simply become
B ( z ) = B 0 tanh ( z δ * ) e x ,
(24)
J ( z ) = B 0 μ 0 δ * sech 2 ( z δ * ) e y .
(25)
Likewise, we also apply curve fitting to obtain the following approximations for the anisotropic temperature components:
T ezz ( z ) T e 0 1 + 0.22 ( T e | | 0 T e 0 1 ) 2 / 3 sech 2 ( z δ ) ,
(26)
T eyy ( z ) T e 0 1 + 0.41 ( T e | | 0 T e 0 1 ) sech 4 ( z k δ ) ,
(27)
where
k = 1 0.85 + T e 0 / T e | | 0 .
It should be noted that Eqs. (26) and (27) are evaluated with δ given in Eq. (10), and not δ * in Eq. (23).
Based on the approximations for B x ( z ) and T ezz ( z ), we apply the force balance constraint in Eq. (7) to determine the approximation for n(z) in Eq. (28), including the pressures of both the electron and ion fluids. From the black dashed curves in Figs. 5(e), 5(k), and 5(q), the validity of this approximation is verified. Finally, given the form for n(z) in Eq. (28), the profile of Φ is approximated in Eq. (29) using the Boltzmann density scaling imposed through Eq. (21) on the ions,
n ( z ) ( T i + T e 0 ) n 0 + ( B 0 2 B 2 ( z ) ) / ( 2 μ 0 ) T i + T ezz ( z ) ,
(28)
e Φ ( z ) T i log ( n ( z ) n 0 ) .
(29)

Again, all of the approximate profiles in Eqs. (23)–(29) are illustrated by the black dashed lines in Fig. 5 against the numerical profiles. In particular, the approximations for n(z) and Φ ( z ) were derived by assuming fluid force balance in the z-direction. Thus, the validation of these approximations demonstrates that the numerical profiles in fact honor fluid force balance also for the cases where Φ ( z ) 0.

In this section, we explore the effects of a non-monotonic electrostatic potential. As an example, the profile of Ez in Fig. 6(a) is now permitted to include multiple sign reversals as a function of z, corresponding to the potential in Fig. 6(b). The inner electric fields pointing outward from z = 0 can trap electrons yielding a new class of electron orbits of the type illustrated by the black electron trajectory in Fig. 6(c). In its xy-projection shown in Fig. 6(d), the trajectory is dominated by a circular cyclotron motion around the Bz magnetic field. For this new class of Ez-trapped electrons, they all cross the z = 0 plane, and we therefore also characterize these as meandering. In what follows, it will be detailed how the orbit topology map in Fig. 6(c) is obtained and how the Ez-trapped region splits the yellow regions of the cyclotron orbit (which before were continuous across z = 0 ).

FIG. 6.

(a) and (b) Illustrative profiles of E z ( z ) and Φ ( z ) yielding Ez-trapping of meandering electrons. (c) Orbit topology map in the (xT, zT)-plane, where the black trajectory provides an example of an Ez-trapped electron. (d) (x, y)-projection of the trapped electron orbit.

FIG. 6.

(a) and (b) Illustrative profiles of E z ( z ) and Φ ( z ) yielding Ez-trapping of meandering electrons. (c) Orbit topology map in the (xT, zT)-plane, where the black trajectory provides an example of an Ez-trapped electron. (d) (x, y)-projection of the trapped electron orbit.

Close modal

Similar to the analysis in Sec. II, for the present configuration, the orbit topologies can be understood by analyzing Φ eff introduced in Eq. (16). A 2D profile of Φ eff ( x T , z T ) is shown in Fig. 7(c), with the location of two representative cuts marked and displayed in Figs. 7(a) and 7(b), respectively. For x T / δ = 7 in Fig. 7(a), three wells are observed, where the central well confines the new class of meandering electrons. The two wells on either sides correspond to the regular cyclotron orbits. The local peaks of Φ eff marked by the red and black circles, respectively, can be found as the roots of Φ eff / z = 0. As a function of xT, we denote the roots with z < 0 as z l 1, defining the line marked l1 in Figs. 7(c) and 7(d). In accordance with Fig. 7(a), the line marked l2 in Figs. 7(c) and 7(d) is then obtained by identifying the value, z l 2, for which Φ eff ( x T , z l 2 ) = Φ eff ( x T , z l 1 ). By this procedure, the orbit topology map in Fig. 6(c) is readily obtained as a function of the turning point coordinates (xT, zT).

FIG. 7.

(a)–(c) Illustrations of the effective potential Φ eff, where the middle well emphasized in the cut in (a) causes Ez-trapping of electrons. (d) Color contours of J z with the common normalization, J z = e / ( 2 π ) v z d z, applied both for cyclotron and meandering electrons.

FIG. 7.

(a)–(c) Illustrations of the effective potential Φ eff, where the middle well emphasized in the cut in (a) causes Ez-trapping of electrons. (d) Color contours of J z with the common normalization, J z = e / ( 2 π ) v z d z, applied both for cyclotron and meandering electrons.

Close modal

In Sec. II, we applied the normalization in Eq. (6) to ensure that J z changes smoothly across the bifurcation lines in the (xT, zT)-plane. However, that normalization does not yield smooth changes for the present scenario including the electrically trapped electrons. Instead, as a first step in Fig. 7(d), we apply the common normalization of J z = e / ( 2 π ) v z d z. In Fig. 7(d), it is observed that the region of electrically trapped meandering orbits (in between the cyclotron regions) are characterized by low values of J z. Along the bifurcation lines l1 and l2, we record the separate values, J z , mea and J z , cyc, corresponding to the two orbit types. As a function of the position along the combined bifurcation line, J z , mea increases monotonically, whereas J z , cyc has a global minimum ( J z , cyc = 0 ) where l1 and l2 meet. Given J z , mea varies monotonically, we may then consider J z , cyc as a function of J z , mea, as shown in Fig. 8(a). This function is important because it informs how J z , mea of the meandering orbits maps onto J z , cyc of the cyclotron orbits where the electrons cross the bifurcation line.

FIG. 8.

(a) For positions along the combined bifurcation line, J z , cyc of the cyclotron orbits is plotted as a function of J z , mea for the meandering electrons. The black dashed line represents J z , cyc = J z , mea / 2, applicable away from the region influenced by Ez-trapping. (b) Φ eff is displayed as a function of J z , mea along the l1 bifurcation line, important for the boundary condition of v x 2 for globally trapped electrons. (c) Color contours of J z, where, for the meandering region, we apply J z = J z , cyc [ J z , mea ( x T , z T ) ], where the mapping J z , cyc ( J z , mea ) is defined in (a). Particular contours of J z are highlighted by the red lines, and illustrative electron orbits at which the turning points follow, the contours of J z are included. (d) Zoom-in view of the central region of (c).

FIG. 8.

(a) For positions along the combined bifurcation line, J z , cyc of the cyclotron orbits is plotted as a function of J z , mea for the meandering electrons. The black dashed line represents J z , cyc = J z , mea / 2, applicable away from the region influenced by Ez-trapping. (b) Φ eff is displayed as a function of J z , mea along the l1 bifurcation line, important for the boundary condition of v x 2 for globally trapped electrons. (c) Color contours of J z, where, for the meandering region, we apply J z = J z , cyc [ J z , mea ( x T , z T ) ], where the mapping J z , cyc ( J z , mea ) is defined in (a). Particular contours of J z are highlighted by the red lines, and illustrative electron orbits at which the turning points follow, the contours of J z are included. (d) Zoom-in view of the central region of (c).

Close modal

In Fig. 8(c), we again evaluate color contours of constant J z, but now with the modification that for the meandering part of the (xT, zT)-plane, we instead display contours of J z , cyc [ J z , mea ( x T , z T ) ], where J z , cyc ( J z ) is the function shown in Fig. 8(a). We hereby obtain a map of J z ( x T , z T ), which is continuous across the bifurcation lines. Again, for the meandering part of the (xT, zT)-plane, the contours now do not represent the actual values of J z. Rather, the contours provide a mapping between the orbit coordinates (xT, zT) to the value of J z a particular electron had as it first started its journey from the asymptotic distribution into the current sheet. A zoomed in view is provided in Fig. 8(d).

The red lines in Figs. 8(c) and 8(d) highlight particular contours of constant J z. We observe how the turning points of the displayed orbits follow these contours. The blue orbit [only in Fig. 8(c)] is of the type explored in Sec. III [like the red orbit in Fig. 2(g)]. Meanwhile, the black orbit in Figs. 8(c) and 8(d) provides an example where an electron initially follows a regular cyclotron orbit and then transitions into the electrically confined orbit type. In turn, this is different from the confined cyan orbit, which does not reach the bifurcation lines and remains confined to the central region of the current sheet.

To understand the boundaries of the confined orbits, in Fig. 7(c), we notice the well in Φ eff as a function of xT for z T 0. The confined electrons are being reflected in this well before reaching the bifurcation line, l1. As displayed in Fig. 8(b), we may evaluate Φ eff along the l1 line as a function of J z , mea. This profile, Φ eff l 1 ( J z , mea ), has a minimum at J z , mea *, where for the present configuration, log 10 ( J z , mea * ) 1. As shown in Figs. 8(b)–8(d), the part of the bifurcation line with J z , mea < J z , mea * is labeled l 1 A. For an electron to be globally confined it must have J z , mea < J z , mea *, and its value of e Φ eff ( x T , z ) + m e ( v x 2 + v z 2 ) / 2 must be less than Φ eff l 1 A ( J z , mea ), displayed in Fig. 8(b).

To obtain (xT, zT) as a function of ( z , v y , v z ), we can again use Eqs. (18) and (19). In turn, with the map in Figs. 8(c) and 8(d), we may then evaluate J z ( z , v y , v z ). The color contours J z ( v y , v z ) in Figs. 9(a)–9(c) are obtained for z / δ { 0.3 , 0.15 , 0 }, respectively. The location z / δ = 0.3 of Fig. 9(a) is outside the region of local trapping by Ez, and the profile of J z ( v y , v z ) is thus similar to that observed in Fig. 3(c). Meanwhile, as shown in Figs. 9(b) and 9(c), for z 0 and v z 0, large values of J z are observed corresponding to Ez-trapped electrons with trajectories similar to the black trajectory in Figs. 8(c) and 8(d). Using Eq. (4), we may again evaluate f ( z , v ). The distributions in Figs. 9(d)–9(f) are obtained for an ambient distribution with T e | | 0 / T e 0 = 4. For the location at the center of the current sheet, the enhanced values of J z for v z 0 causes significant reductions in f, yielding the observed double peaked distributions in the (vy, vz)-plane.

FIG. 9.

(a)–(c) Color contours of log 10 ( J z / J z 0 ) as a function of (vy, vz) for z / δ { 0.3 , 0.15 , 0 }. (d)–(f) Solutions for f ( z , v ) obtained from Eq. (4) using an f0 with T e | | 0 / T e 0 = 4. Color contours are shown of log 10 [ f / f 0 ( v = 0 ) ] at vx = 0 as a function of (vy, vz) also for z / δ { 0.3 , 0.15 , 0 }.

FIG. 9.

(a)–(c) Color contours of log 10 ( J z / J z 0 ) as a function of (vy, vz) for z / δ { 0.3 , 0.15 , 0 }. (d)–(f) Solutions for f ( z , v ) obtained from Eq. (4) using an f0 with T e | | 0 / T e 0 = 4. Color contours are shown of log 10 [ f / f 0 ( v = 0 ) ] at vx = 0 as a function of (vy, vz) also for z / δ { 0.3 , 0.15 , 0 }.

Close modal

The 1D current layers explored in this section have characteristics relevant to magnetic reconnection. During magnetic reconnection, electron pressure anisotropy typically develops within the reconnection inflow regions.29 In particular, for anti-parallel reconnection, this upstream pressure anisotropy supports the current layer of meandering electrons that develops within the electron diffusion region (EDR).28,30,31 As an example, in Figs. 10(a)–10(f), we display various profiles obtained in a fully kinetic simulation. The data correspond to the case with an ion to electron mass ratio m i / m e = 1836, and an upstream normalized electron pressure β e = 2 4. The run was explored in Ref. 28, where a more complete account of the simulation setup is given.

FIG. 10.

(a)–(f) Profiles from a kinetic simulation of anti-parallel magnetic reconnection. The details describing the numerical run with m i / m e = 1836 and β e = 2 4 can be found in Ref. 28. (g) Profile of E z ( z ) applied in the 1D current sheet model. (h)–(j) Profiles obtained with the 1D model for T e | | 0 / T e 0 = 4 using the iterative scheme of Sec. III A. In the 1D model, the current is driven by the anisotropy, and the similarities between the profiles in (d)–(f) and those in (h)–(j) highlight previous results on how EDR current channels in reconnection similarly are driven by electron pressure.

FIG. 10.

(a)–(f) Profiles from a kinetic simulation of anti-parallel magnetic reconnection. The details describing the numerical run with m i / m e = 1836 and β e = 2 4 can be found in Ref. 28. (g) Profile of E z ( z ) applied in the 1D current sheet model. (h)–(j) Profiles obtained with the 1D model for T e | | 0 / T e 0 = 4 using the iterative scheme of Sec. III A. In the 1D model, the current is driven by the anisotropy, and the similarities between the profiles in (d)–(f) and those in (h)–(j) highlight previous results on how EDR current channels in reconnection similarly are driven by electron pressure.

Close modal
To compare the results for the 1D current sheet to the numerical results for reconnection, we must first establish a connection between δ in (10) and the electron skin depth d e = m e / ( μ 0 n e e 2 ), used as the characteristic length scale in the kinetic simulation. From Fig. 1(b) of Ref. 28, it is seen that T e | | 0 / T e 0 = 4 just upstream of the EDR, which is useful for relating δ and de. In fact, using Eqs. (8)–(10), we find that
δ = 2 m e T e | | 0 T e 0 e 2 μ 0 n 0 ( T e | | 0 T e 0 ) = 2 T e | | 0 T e 0 ( T e | | 0 T e 0 ) d e 0 .
Thus, with T e | | 0 / T e 0 = 4, we obtain δ = 4 / 3 d e 0, where d e 0 is the electron skin depth as observed just upstream of the EDR in the simulation. Using this relationship, in Figs. 10(a)–10(f), all length scales are normalized with respect to δ.

The full profile of E z ( x , z ) from the kinetic simulation is shown in Fig. 10(a), normalized by E 0 = E δ / ( e δ ), where E δ is evaluated using Eq. (8). As is typical for simulations of anti-parallel reconnection,32 the cut of E z ( z ) in Fig. 10(c) for x = 0 has a structure similar to that analyzed for the 1D current layer in Fig. 6(a). The total electron current density Je is shown in Fig. 10(b), normalized by J0 in Eq. (11). A profile cut at x = 0 is shown in Fig. 10(d), where a bifurcated double peaked structure in Je is clearly observed. Meanwhile, the similar cut across the number density profile in Fig. 10(e) is mostly uniform.

In the above analysis, we observed how applying the simulation Ez-profiles in the 1D model causes double peaked structures in the model phase space distribution. To help visualize these structures both for the simulation and the model, we compute the reduced phase-space distribution g ( v z ) = f ( v ) d v x d v y. In Fig. 10(f), we display g ( z , v z ) for a cut across the EDR at x = 0. A prominent electron–hole structure centered on z = 0 is observed, similar to those studied in Ref. 32.

Predictions of the 1D current model are evaluated for T e | | 0 / T e 0 = 4, while imposing the Ez-profile shown in Fig. 10(g). Based on the iterative scheme detailed in Sec. III A, we obtain the profiles of J e y ( z ), n(z), and g ( z , v z ) shown in Figs. 10(h)–10(j), respectively. While some differences between the kinetic simulation profiles and those of the 1D current layer are clearly present, we notice the similarity in the profiles of J e y ( z ) as well as g ( z , v z ). It should be emphasized again that in the 1D model the results were obtained by imposing the profile of Ez causing the bifurcated current layer and electron–hole structure. The self-consistent 1D current layers in Sec. III B did not develop these features, and it is possible that the bifurcated current layer is unique to the reconnecting geometry. However, the similarity between J e y ( z ) of the simulation and the 1D model emphasizes how the reconnection current layer is mainly driven by the electron pressure anisotropy that develops in the reconnection inflow regions.28,30,31 Future work will explore in more detail the applicability of the 1D model to anti-parallel reconnection.

In the present paper, we have developed a framework for understanding and modeling 1D current layers including a small normal magnetic field. First, it should be noted that the familiar Harris sheet solution is not compatible with any normal magnetic field, as such a field causes thermal streaming of particles across the current sheet. Mathematically, the underlying kinetic solution of the Harris sheet is parameterized in terms of py in Eq. (13).4 However, through Eq. (12), we notice how py becomes a function of x for any finite Bz. This x-dependency of py imposes that any 1D solution independent of x must be also independent of py. With these observations, it is then clear that the Harris-type solution is only valid for the case where Bz is exactly zero.

Breaking with the Harris-approach of parameterizing the solution in terms of the canonical momentum, py, we instead use that py is a constant of motion variable to derive closed form expressions for the J z v z d z action integral. In contrast to the magnetic moment, J z is a well-conserved adiabatic invariant. Based on this observation and with the development of numerical routines for evaluating J z ( z , v y , v z ), we explore the class of 1D solutions simply expressed by the form f ( x , v ) = f 0 ( U , J z ). Here, f0 is the asymptotic electron distribution, and U is the total energy of the electrons. It should be noted that at bifurcation points where the orbit topology changes from the cyclotron type into the meandering type, the values of J z change abruptly. However, these changes are readily characterized and accounted for in the model.

Based on the framework outlined above, for given profiles of B x ( z ) and Φ ( z ), the full solutions for f ( z , v ) are readily obtained. This, in turn, facilitates a numerical scheme to determine the profiles of B x ( z ) and Φ ( z ), consistent with Ampère's law and the condition of quasi-neutrality. While not imposed numerically, we find that the converged kinetic solutions are in fluid force balance across and along the current sheet, validating the numerical approach. Given the finite values of Jy and Bz, it is clear that J × B-forces are present in the x-direction along the current layer. In the self-consistent solution, these forces are balanced by thermal forces associated with the upstream pressure anisotropy. Concisely, the overall force balance in the x-direction is expressed through the marginal fire-hose condition in Eq. (3). This equation is fundamental to the 1D current layer, as it parameterizes how the pressure anisotropy regulates B0. In other words, it is the upstream pressure anisotropy that controls the value of the integrated current across the current layer. Our approach is similar to previous work in the literature,22,23,33 but is perhaps more general. For example, in contrast to Ref. 22, we do not include any fluid closure assumptions for evaluating the electron current profile.

For the case of isotropic ions with temperature T i 0 and bi-Maxwellian electrons with asymptotic parallel and perpendicular temperatures T e | | 0 and T e 0, the solutions can be parameterized in terms of the temperature ratios T i 0 / T e | | 0 and T e 0 / T e | | 0. No other parameters influence the mathematical form of the solutions. As a function of T i 0 / T e | | 0 and T e 0 / T e | | 0, closed form numerical approximations are obtained across the current sheets of all essential fluid quantities. These approximations provide quantitative insight into how 1D current layers are affected by the asymptotic boundary conditions and may become useful to the analysis of spacecraft data or future theoretical studies of the present type of 1D current layer.

The numerically identified self-consistent profiles of Φ ( z ) are monotonic in | z |. However, from reconnection studies, it is known that electron current layers can develop including a non-monotonic profile of Φ ( | z | ). We therefore generalize the 1D model to include such more general electrostatic potentials. In particular, kinetic simulations of anti-parallel magnetic reconnection include profiles of Φ ( z ), which yield electrically trapped electron trajectories. By applying profiles of Φ ( z ) of this nature in the 1D model, a range of features of the reconnection geometry are reproduced. Among these features is the creation of bifurcated double-peaked layers with a width on the order of the electron skin depth, c / ω p e.

Future studies will clarify the applicability of the 1D model to the structure of the current layers in anti-parallel reconnection. Preliminary results (not included here) suggest that although the inductive Ey reconnection electric field is not considered in our geometry, the approximations derived for J z remain valid. In fact, the new framework in combination with the electron distribution model in Ref. 29 appears to provide an accurate account of the Jy current profile as well as the on-diagonal electron pressure components within the reconnection inflow and electron diffusion region. Furthermore, the model may be generalized to accommodate finite values of Ey by imposing the previous observed rotation of the central reconnection current layer into the outflow directions. This, in turn, can account for the main off-diagonal electron stress components discussed in Ref. 28. The details of these findings will be reported in separate publications.

The author acknowledges discussions, comments, and suggestions by Young Dae Yoon, Samuel Greess, Abhishek Mhatre, and William Daughton. This work was supported in part by H. I. Romnes Faculty Fellowship by the UW-Madison Office of the Vice Chancellor for Research and Graduate Education.

The author has no conflicts to disclose.

Jan Egedal: Writing – original draft (lead).

The data that support the findings of this study are available from the corresponding author upon reasonable request.

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