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Chapter 4
KINETIC PHENOMENA IN THE PLASMA
During the passage of an electric current, a plasma is in non-equilibrium. The deviation from thermodynamic equilibrium in a TIC is most pronounced near the electrodes and is comparatively slight deeper within the plasma. With small deviations from equilibrium, the particle and energy fluxes in the plasma are determined by the gradients of the plasma parameters, i.e., by the gradients of the particle densities, the particle temperatures, and the potential.
In this chapter expressions are derived which relate these fluxes to the gradients of the plasma parameters. The case of a weakly ionized plasma is considered, in particular, where the state of the neutral gas is not dependent on the current, on the density and temperature of the charged particles, or on the electric field. Equations are formulated, however, which are subsequently used to find the distribution of these variables in the TIC interelectrode space.
The chapter is concerned primarily with the calculation of the state of a weakly ionized TIC plasma. More detail on the kinetics of plasmas in general can be obtained from monographs devoted specifically to this problem. In particular, a survey of the most recent investigations of plasma kinetic scan be found in [1].
1. The Kinetic Equation
The state of a gas is totally characterized by the distribution function f(v@, r@, t), which is equal to the average number of particles @ which have coordinates from x to x + dx, from y to y + dy, and from z to z + dz; and velocity components from vx to vx + dvx, from vy to vy + dvy , and from vz to b. These particles are therefore in a volume element of coordinate space d3r = dxdydz and of velocity space d3v = dvxdvydvz, i.e.,
?
Using the distribution function, one can determine any characteristic of the gas. For example, the particle density
n(r@, t) is expressed as
(1.1)
Any particle function of velocity
X(v) at a given point of space can be averaged over velocity by the relation
(1.2)
to obtain the average value of the function at that point. For example, average energy is
(1.3)
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Since the distribution function
f(v, r, t) is the particle density in a space of six dimensions with coordinates vx, vy, vz, x, y, and z, then, in the absence of collisions, it should satisfy the continuity equation
(1.4)
where
I@ is the flux of particles in the six-dimensional space.Equation (1.4) is a generalization of the ordinary continuity equation for a three-dimensional space. The flux of particles with a given velocity
v@ in ordinary space, as is well known, is given by ir@ = fdr@ / dt = fv@. The flux in velocity space is accordingly iv@ = fdv / dt = Ff@ / m, where F@ is the external force acting on the particles. Vector i@ is the sum
(1.5)
Calculating
div i@ in the usual manner as the sum of the partial derivatives of projections ia to the coordinate axes, we find that
(1.6)
The subscripts
r and v denote differentiation by r and v, respectively.The force ±
eE@ (due to the electric field E@) and the Lorentz force ± e(v@ x H@)/c (due to the magnetic field H) act on a particle with charge ± e. Therefore, in general, the force on a particle is
(1.7)
where the upper sign is taken for ions and the lower sign is taken for electrons. When calculating the right side of (1.6), we use the fact that the velocity
v@, coordinate r@, and time t are independent variables in the continuity equation (1.4).It is easy to show from (1.7) that
divvF@ = 0. As a result, from (l.4) and (1.6), we obtain the following equation for the distribution function f(v@, r@, t):
(1.8)
Equation (1.8) is valid if the particles considered do not collide with each other or with other particles. In the presence of collisions, the particle flow is no longer continuous, because particles change their velocity sharply with each collision , i.e., they disappear at specific points of velocity space and appear at other points. Therefore, the change of the distribution function due to collisions must be taken into account separately. By denoting the change of the distribution function due to collisions by
I{f}, we obtain the following equation for the distribution function:
(1.9)
Equation (1.9) is called the kinetic equation or the Boltzmann equation. The right hand term
I{f} is called the collision term of the kinetic
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equation.
We note that the effects of "external" forces and of collisions on particle motion are taken into account in the kinetic equation by essentially different methods. It is assumed that collisions occur instantaneously at a given point of space
(with coordinates x, y, and z) and that the only result of a collision is a change in the particle velocity (and in the general case, of the internal state as well). Therefore, the kinetic equation is valid for those cases where the collision time D t is much less than the time T during which external forces vary appreciably, and where the change of the particle coordinate during collision, D r, is much less than l (where l is the distance over which there is significant variation of the external fields).When calculating the collision term, it is also usually assumed that the external fields do not affect the collision process, i.e., that the interaction forces between the particles are considerably greater during collision than the external field
F@. (This effect, however, can be taken into account if necessary.)The kinetic equation is a classical equation. For a particle moving in a gas to be regarded classically, it is necessary that its de Broglie wave length be considerably less than the mean free path of the particles, i.e., that the condition
h/mv << l be fulfilled, or accordingly, that energy E >> h@/t . If this condition is fulfilled, one may assume that the particle moves between collisions according to the laws of classical mechanics. As for the collision term, generally speaking, it must be calculated using quantum mechanics.Thus, the use of the kinetic equation requires fulfillment of a number of conditions. In the cases considered here, these conditions are usually fulfilled.
As already noted above, Coulomb interactions in the plasma, strictly speaking, are not binary interactions, because very many charged particles are included in a Debye sphere
(radius LD). Therefore, a specific particle at any given moment of time interacts with many charged particles rather than just one.However, when the temperature of the electrons and heavy particles are close to each other, and oscillations in the plasma do not differ strongly from the thermal noise, the results of precise theory (see, for example, [2-4]) coincide with the results of the theory of binary collisions, in which the Coulomb interaction is "cut-off" at a distance equal to
LD.*During Coulomb collisions, the main interaction between particles occurs within a distance of the order of
LD. In this case, the interaction energy is of the order of e 2/LD. This value is usually small compared to the kinetic energy mv2/2 of a colliding particle, so that the particle velocity v@ usually changes insignificantly as a result of the collision. Therefore, during Coulomb collisions, the charged particles seem to diffuse within velocity space. This concept of diffusion for the electron motion in velocity space is used extensively (see §§5 and 6 of this chapter). The condition for this concept to be applicable__________
*An exception is the case where the particle distribution function is unstable and the oscillations in the plasma grow, so that the oscillation amplitude may become considerably higher than the thermal noise amplitudes
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is the fulfillment of the inequality
(mv2/e2)LD >> 1. We note in this case the Coulomb logarithm ln@ = ln{(mv2/e2)LD}, which figures in equation (3.2.10) for the cross section Qp for Coulomb collisions, is large compared to unity.
2. Solution of the Kinetic Equation in the Relaxation Time Approximation
The kinetic equation, including the effect of collisions, is an integral-differential equation, and in general, can not be solved analytically. The simplest kinetic equation to be solved is the case of a weakly ionized, inhomogeneous plasma, where the density and temperature of the particles hardly change over the length of a mean free path
(l dn/dx « n and l dT/dx « T), and where the electric field E@ in the plasma is sufficiently weak so that, first, the energy acquired by a particle in the field over the length of a mean free path is small compared to the thermal energy of the particle (eEl « kT), and second, the charged particles manage to effectively exchange the energy acquired by them from the field.*The solution of the kinetic equation with these assumptions, for steady-state (distribution function not dependent on time), is considered in this section.
If the particle density and temperature gradients and the potential gradients are weak, and if the energy acquired by charged particles from the field is dissipated rapidly, the particle velocity distribution function
f(v@) does not differ greatly from the Maxwellian distribution function. This permits a solution of the problem by iterative approximations. To do this, let f(v@) be represented as a sum
(2.1)
where
f(1)(v@) is a minor non-equilibrium addition to the distribution function and fM(v) is a Maxwellian distribution function:
?
Assume also that the addition
f(1)(v@) to the distribution function contains the electric field E@ and the terms in gradr only to first order.In zero approximation, i.e., disregarding small values, only the term
(e/mc)(v@ x H@) gradv fM(v), which is equal to zero, remains on the left side of the kinetic equation (1.9), because gradv fM(v) = (v@ /v)dfM(v)/dv and v@ (v@ x H@) = 0. Substitution of fM(v) into the right side of the kinetic equation also yields zero, because the collisions do not disrupt the Maxwellian distribution. @________
*This condition is more strict for electrons, which lose a very insignificant fraction of their energy during collisions with heavy particles as a result of their small mass. In a weakly ionized TIC plasma, if the electron concentration is adequate
(n ³ 1012 cm-3), the energy obtained by them from the field is dissipated primarily by electron-electron collisions. In this case, the electric field leads to a variation in the temperature of the electron gas, whereas the electron distribution function itself deviates comparatively little from the Maxwell distribution (see §6).@
For the electron—atom collisions considered in this section, this condition is fulfilled, because the atoms are assumed to be at rest during collisions. If, however, the motion of the atoms were taken into account, the collision
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Continuing the approximation, retaining terms of first order, we obtain an equation for calculating
f(1)(v@):*
(2.2)
By substituting
fM(v) into the left side of (2.2), equation (2.2) transforms to
(2.3)
where
p = nkT is the pressure, n is the density of particles of a given specie, and w c@ = eH@/mc is a vector, equal in modulus to the cyclotron frequency w c.To solve equation (2.3), it is necessary to have an explicit expression for the collision term
I{ f(1)(v@)}. In general, the collision term is in the form of an integral of the desired distribution function f(1)(v@). Therefore, equation (2.3) is an integral equation. Only in some cases it can be solved exactly. Of these cases, those of greatest present interest are those where charged particles collide with each other only rarely (compared to collisions with constant scattering centers) and where scattering centers may be assumed immobile in view of their large mass. @ This is the case, in particular, for a weakly ionized plasma with low electron densities, where electron collisions with neutral atoms are the main scattering mechanism.Variation of the distribution function due to particle collisions with infinitely heavy scattering centers can be written in the following form:
(2.4)
where
N is the density of the scattering centers, s (v, q ) is the differential scattering cross section, v@' is the particle velocity after scattering, q is the scattering angle, and dW = 2p sinq dq is the element of solid angle. The collision term in (2.4) is represented in the form of the difference of two values.The term
vNf(v@ ) ò s (v, q ) dW is the decrease in the number of particles in a state with velocity v@ as a result of collisions, and in this case, the value of vNs (v, q ) is the particle scattering probability for deflection by angle q from the initial direction of motion (Fig. 4.1). Integration over dW denotes integration over all directions of electron velocity v@' after scattering.____________
term
Iea would be distinct from zero if the electron and atomic temperatures were different.*Expression (2.1) represents the first two expansion terms in the Chapman-Enskog method
[7]. Integral equations of the same form as (2.2) are obtained for expansion terms of higher order.@
A gas of non-interacting particles, scattering from fixed centers, is usually called a Lorentz gas. Therefore, the approximation used is also called the Lorentz approximation.
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Fig. 4.1
The second term
vNò f(v@')s (v,q ) dW corresponds to the increase of the number of particles with velocity v@' due to collisions. Integration over dW denotes integration over all velocities v@' prior to collision, while the value of vNs (v,q ) is the probability that the particle will move from a state with velocity v@' to a state with velocity v@. As can be seen from Fig. 4.l, the same scattering angle and, consequently, the same value of cross section @ corresponds to the transition from state s (v,q ).*If there are weak gradients of temperature, density, and potential, a solution of the kinetic equation (2.3) can be found in the form
(2.5)
Here c
@(v) is a vector dependent only on the velocity modulus v, which is calculated as a result of solving the kinetic equation, and q is the angle between the direction of particle velocity v@ and the direction of vector c @. The function fM(v) is singled out on the right side of (2.5) for convenience in writing the subsequent expressions.Having substituted (2.5) into (2.4), we obtain
(2.6)
To calculate the integral in (2.6), we can use the polar coordinate system and direct the polar axis
x along the particle velocity vector v@ before collision (Fig. 4.2). Then
(2.7)
By substituting (2.7) into (2.6) and taking into account the fact that the terms containing
sinq and cosq do not contribute to the result during integration over angle q , we obtain
(2.8)
where
(2.9)
is the inverse momentum relaxation time introduced above (see formula
(3.1.13)).
To find the non-equilibrium component to the distribution function,
_____________
*The equivalence of the differential cross section s
(v,q ) for direct and inverse transitions is a result of the principle of detailed balance (see §5, Chapter 3).
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Fig. 4.2
we substitute expression (2.8) for the collision term into equation (2.3). In this case, using (2.5) and the relation
(v@ x w c)gradvf(1)(v@) = - fM(v@) v@ [c @ (v) x w c ], which follows from (2.5) (see, for example, [5]), we find
(2.10)
where the
+ and - signs, as before, correspond to the positive and negative charges on the particle.Formula (2.10) determines vector c
@. In particular, it is obvious that vector c @ is dependent only on the velocity modulus v, which justifies the assumption made above.
3. Transport Equations and Kinetic Coefficients in the Relaxation Time Approximation. Electron Current and Electron Energy Flux in a Weakly Ionized Plasma
The electron current density
je@ is equal to the directional average of the electron velocity multiplied by the electron density and charge. The kinetic energy flux density Sek@ of the electrons is equal to the average energy transferred by one electron (averaged as in formula (1.2)) multiplied by the electron density.Expressions for electron current and electron energy flux. Electron current
je@ and kinetic energy flux Sek@, transferable by electrons, are calculated in the following manner using the electron velocity distribution function:
(3.1)
(3.2)
With this definition the forward direction of electric current is assumed to be in the direction of motion of the electrons, rather than that of the ions. In this case,
je@ = +eie@ and ji@ = - eii@, where ie@ and ii@ are the flux densities of the particles, electrons and ions respectively.In this section we derive expressions for
je@ and Sek@ in the absence of a magnetic field.Calculating
je@ and Sek@ only the non-equilibrium component to the distribution function fe(1)(v@), instead of fe(v@), need be substituted into (3.1) and (3.2), because naturally there is no current or energy flux in the equilibrium state.
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Since the non-equilibrium component to the distribution function is proportional, in this case, to both
(eneE@ + gradPe) and nekgradTe, there are two contributions to the current je@ that are proportional to these quantities. Denoting the proportionality constants by m e and Ke(T)m e, respectively, we write the expression for the electric current transported by the electrons in the following form:
(3.3)
Coefficients m
e and Ke(T) are called the mobility and the thermal-diffusion ratio, respectively. The value of s = em ene, as indicated above, is the electrical conductivity of the plasma.When calculating the kinetic energy flux Sek@ it is convenient to separate terms proportional to electron flux je@/e and to the electron temperature gradient:
(3.4)
Here k
e is the thermal conductivity of an electron gas. Equations (3.3) and (3.4) are called the transport equations for electron current and electron kinetic energy flux, and the values of m e, Ke(T) and k e are the kinetic coefficients. In the relaxation time approximation, the kinetic coefficients are calculated using the following expressions:
(3.5)
(3.6)
(3.7)
In formulas (3.5)—(3.7), t
p is the momentum relaxation time and the symbol < > denotes averaging over the Maxwellian distribution function, according to (1.2). Expressions (3.5) and (3.6) for mobility and the thermal-diffusion ratio are obtained directly by substituting (2.10) into (3.1) (with w c@) and by integration by angular variables, i.e., over dW . To obtain expression (3.7) for the electron thermal conductivity, it is convenient to use the fact that the flux density of thermal conduction k e grad Te is the transport of energy by the particles in the absence of current, i.e., where je@ = 0. In this case, as follows from(3.3),
?
Having substituted this relation into (2.10), and the result into (3.2), and having performed integration over angles, we obtain (3.7). Typically the integrand in (3.7) is a function that changes sign: If
je@ = 0, two counter particle-flows pass through the plasma which counteract each other. The kinetic energy flux Sek@ is non-zero in the presence of a temperature gradient, because the faster particles moving in the direction of lower temperature transfer greater kinetic
89
energy than slow particles moving in the other direction. The explicit expressions for the kinetic coefficients are determined by the dependence of the relaxation time t
p on velocity v.Expressions for the kinetic coefficients and for the fluxes with various dependencies of relaxation time and of mean free path on energy. First, consider the case where the relaxation time t p is not dependent on v. In this case,
?
and, accordingly,
(3.8)
At t
p = const, the electron distribution function fe(v@ ) in the electric field is a Maxwellian distribution, shifted in velocity space an amount equal to the average drift velocity vde@, the same for all electrons:
(3.9)
Actually, taking into account the low value for the drift velocity
vde@, from (3.9) we find that
(3.9a)
By comparing (3.9a) to (2.1) and (2.10)
(at w c@ = 0 and gradTe = 0) we find
(3.10)
i.e.,
vde@ is actually not dependent on v. If there is a temperature gradient, the distribution function is no longer represented in the form of (3.9).The value of thermal conduction k
e at t p = const is obtained from (3.7), using the fact that in this case Ke(T) = 0:
(3.11)
If the relaxation time t
p is dependent on v, the thermal-diffusion ratio is distinct from zero and the thermal-diffusion current
(3.12)
is not equal to zero.
According to (3.6), the sign of the thermal-diffusion ratio and the direction of the thermal-diffusion current are determined by the nature of the dependence of
t p on v: Ke(T) is positive if t p is an increasing function of v, and negative in the opposite case.
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When relaxation time is proportional to a power of v, i.e., when the mean free path is given by
(3.13)
calculation of integrals (3.5)—(3.7) leads to the following results
(3.14)
(3.15)
(3.16)
where
ve@ = <ve> = (8kTe/p m)1/2 is the average electron velocity of the Maxwellian distribution, re = 1/2 corresponds to constant collision time, and re = 0 corresponds to a constant mean free path. In the latter case
(3.17)
since G
(2) = 1.The approximation of a constant mean free path, in particular, corresponds to a model in which particle collisions are treated as the elastic impact of two hard spheres. In this case
lp = l = 1/NQ, where N is the density of the scattering particles and Q is the total elastic scattering cross section, equal to p (ra + rb)2, where ra and rb are the radii of the spheres. This approximation is the one usually used to describe electron scattering from neutral Cs atoms.The general form of the transport equations. Transport equations (3.3)—(3.4) were obtained in the relaxation time approximation. Actually, they are valid independent of this approximation, because in the case of plasma parameter gradients, the particle and energy fluxes are always expressed linearly in the gradients of potential, pressure, and temperature.
The transport equations are often written in a somewhat different form: the gradient of pressure
p = knT can be expressed in terms of density and electron temperature gradients, and the energy flux includes not only the flux of kinetic, but also that of the potential energy of the particles Vje@. In this case,
(3.18)
(3.19)
Here
(3.20)
is the diffusion coefficient, and
Se@ = Se(k)@ + Vje@ is the total energy flux. The relationship (3.20) between the diffusion coefficient and mobility is called the Einstein relation. It is valid if the particle flux is
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expressed linearly by the electric field and the concentration gradient.
4. The Effect of a Magnetic Field on Transport Phenomenon
As indicated above, the Lorentz force
F@ = ± e(v@ x H@ )/c acts on a charged particle moving in a magnetic field. Since F@ ~ (v@ x H@ ) the magnetic field affects particle motion only in the plane perpendicular to H@, not particle motion in a direction parallel to H@. With free motion in a plane perpendicular to the magnetic field, a charged particle would describe a circle with a radius rc = cmv/eH@. If the particle has a velocity vector parallel to the magnetic field, this circle is transformed into a spiral wound on the magnetic lines of force (Fig. 43).Collisions distort this spiral motion. With collisions, the nature of motion is determined by the relationship between rc and the mean free path lp, i.e., by the parameter lp/rc = w ct p where w c = eH/mc, already calculated above, is the cyclotron frequency (the particle rotation frequency along the circumference in the plane perpendicular to H@).
In a weak magnetic field, where w ct p « 1, the particle trajectory is only slightly curved between collisions, because the particle manages to cover only a small fraction of the cyclotron circumference during time t p (see Fig. 4.3a). Curving of the trajectory causes the particle to travel a shorter distance from the scattering center during the free path than if there were no magnetic field. As a result, the equivalent mean free path is decreased. Consequently, the transport coefficients in the plane perpendicular to the magnetic field also are decreased. In a strong magnetic field, where w ct p >> 1 the particle manages to describe many turns of the spiral within time t p. After each collision, the particle begins to describe a new spiral,
Fig. 4.3
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whose axis does not coincide with that of the preceding spiral (Fig. 4.3b).* Therefore, a particle in a strong magnetic field is shifted in a direction perpendicular to
H@ only by collisions. Each collision is accompanied by a displacement of the particle a distance of the order of rc (Fig. 4.3b). Since the extent of the magnetic effect is determined by the parameter w ct p, which is (M/m)1/2 time greater for electrons than for ions, the magnetic field acts on the electrons much more intensively than on ions.Consider the effect of the magnetic field on the electron mobility and the diffusion coefficient for a weakly ionized plasma in the relaxation time approximation. Since the mobility and the diffusion coefficient are related by the Einstein relation, it is sufficient to consider the dependence of only one of these on the magnetic field, for example, the mobility m
e.According to (2.10), the equation for calculation of c
@ (v), in the relaxation time approximation, has the form
(4.1)
Multiplying (4.l) vectorially by w
c@ on the right side and using the property of the dual vector product, (A@ x (B@ x C@ )) = B@ (A@ · C@ ) - C@ (A@ · B@),we find
(4.2)
Upon vector multiplication of (4.1) by w
c@, we obtain
?
Using this, (4.2) becomes
(4.3)
(4.4)
From (4.4), (2.5), and (3.1), we obtain the electron current
je@:
(4.5)
______________________
*Note the characteristic feature of Coulomb collisions in a magnetic field. Since interaction during Coulomb collision occurs at a distance of the order of the Debye length
LD, the interaction time during collision is of the order of w p-1 (where w p = Ö 4p nee2/m@ is the electron plasma frequency).
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It is obvious from (4.5) that in a magnetic field the vectors
je@ and - E@ cease to be parallel. Therefore, mobility m ea b (H) is a tensor and has both diagonal and non-diagonal components in a magnetic field.If the magnetic field is directed along the
z-axis, then, if relaxation time t p is not dependent on velocity, the current components perpendicular to the magnetic field are equal to
(4.6)
(4.7)
Here m
e = et p/me is the electron mobility in the absence of a magnetic field (see (3.8)). The current component jex, as with H = 0, is expressed by the formula jex = - enem eEz. Therefore, for the mobility tensor components m ea b (H), we obtain
(4.8)
(4.9)
(4.10)
If the electric and magnetic fields are mutually perpendicular, current
je@ consists of two components: current components jEe@, directed along the vector -E@, and the so-called Hall current jEh@, directed perpendicular to both the electric and magnetic fields:
(4.11)
It is obvious from (4.11) that the Hall current in strong magnetic fields is considerably greater than current along the electric field but perpendicular to the magnetic field.
In crossed electric and magnetic fields, it is convenient to separate the electric field component
E0@ (parallel to current) from the so-called Hall field EH@ (the field component perpendicular to both current and the magnetic field). Components E0@ and EH@ are calculated from (4.5). If the relaxation time is constant,
(4.12)
In this case, the average electron drift velocity in the direction of
E0@ is equal to vde = -m e E0 and, consequently, is the same as in the absence of a magnetic field. Taking this relationship for E0 and________
If w c » w p, then the electron describes a circle between collisions whose radius is of the order of LD. In this event, the magnetic field begins to affect the nature of the interaction between the particles. Consideration of this circumstance usually leads to a change in the maximum impact parameter for Coulomb collisions.
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Fig. 4.4
substituting it into the first formula of (4.12) we obtain
(4.13)
Fig. 4.4 explains the occurrence of the Hall field in a plasma placed between non-conducting electrodes in an external electric field
E0@. The Hall field occurs due to the accumulation of charged particles near the electrodes, which are shifted toward the electrodes during charged particle motion in crossed electric and magnetic fields. In this case the Hall field EH@ exactly compensates the Lorentz force F@.*In general, when t p is dependent on v, the electron mobility in the plane perpendicular to H@, according to (4.5), is given by the expressions
(4.14)
(4.15)
It follows from (4.14) that a decrease of mobility along the electric field in the presence of a magnetic field perpendicular to it is given by the following expression:
(4.16)
Thus, it follows in particular, that if the length of the mean free path is constant
(lp = vt p = const), then we have
(4.17)
(4.18)
where expression (3.17) is used for the electron mobility m
e with a constant mean free path. Function F(q )@ is shown graphically in Fig. 4.5.In the presence of a magnetic field, the electron diffusion coefficient, like mobility, is a tensor. The diffusion tensor components
Dea b (H) are related to the mobility tensor components m ea b (H)_______________
*To be more general, if the relaxation time t
p is dependent on the electron velocity v, then the Hall field still compensates the Lorentz force-on the average-so that the total current in the direction of the Hall field is zero. In this case, the slow electron flow is directed in one direction, and fast electron flow is directed in another.
95
by the relation
Dea b (H) = (kTe/e)m ea b (H).
Fig. 4.5
5. The Effect of Interelectrode Collisions and Ion Scattering on the Kinetic Coefficients for Electrons
As the degree of plasma ionization increases, electron-ion and electron-electron collisions become important. Electron-ion collisions are an additional mechanism of electron scattering and, therefore, lead to a decrease in the electron kinetic coefficients. Electron-electron collisions play a different role. The total momentum and total energy of the electron system do not change as a result of electron-electron collisions. Nevertheless, electron-electron collisions do affect the magnitude of the electron current and energy flux, because the electron energy distribution depends on the extent of electron-electron collisions. Therefore, if the relaxation time t
p, which characterizes collisions of electrons with atoms and ions, is dependent on energy, the electron-electron collisions change the average value of relaxation time and, consequently, the value of mobility m e.However, electron-electron collisions have a stronger effect on the values of heat conduction k
e and the thermal diffusion ratio Ke(T). Intensive electron-electron collisions lead to a Maxwellian distribution in the coordinate system moving with average drift velocity vde@ of the electron flow (see (3.9)). For this distribution function, k e and Ke(T) are generally equal to zero.* Therefore, electron-electron collisions sharply reduce the electron heat conduction and thermal-diffusion ratio.To see the effect of electron-electron collisions on the kinetic coefficients, consider the values of the mobility m
e, the thermal-diffusion ratio Ke(T), and the thermal conductivity k e for a completely ionized plasma in the absence of a magnetic field:_____________
*This can be shown by substituting (3.9) into (3.2) and by comparing
@ the result with (3.14) where je@ = envde@ and vde@ << Ö kTe/m@.
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(5.1)
The values of m
e, Ke(T) and k e are written so that the coefficients g u, g k, and g k , which are equal to unity without electron-electron collisions, are a measure of this effect. In the latter case, the kinetic coefficients for electrons in a completely ionized plasma are calculated by formulas (3.13)—(3.16), if the mean free path lp(E) = 1/nQp(E) from (3.2.10) is substituted into them. When taking into account electron—electron collisions this way, we obtain g m = 0.582, g k = 0.469, and g k = 0.235 [6]. Therefore it is clear that electron-electron collisions have an important affect on the values of the kinetic coefficients.The kinetic equation in the presence of several scattering mechanisms. If electron—atom, electron—ion, and electron—electron collisions are all present in a plasma, the collision term is the sum of three terms that describe the change of the distribution function due to each kind of collision separately:
(5.2)
The first two terms, which describe electron scattering from atoms and ions, were written in the relaxation time approximation
(t pea and t pei are the electron relaxation times with atoms and ions). The last term, which corresponds to electron-electron collisions, requires special consideration.The characteristic feature of electron—electron collisions is that its analysis requires the motion of both particles to be taken into account. In general, the change of the distribution function for particles
a due to collisions with particles b is given by the expression
(5.3)
Here
va@ and vb@ and va '@ and vb '@ are the velocities of interacting particles before and after collision, respectively; g@ = va@ - vb@ is the relative particle velocity, s (g, q 0) is the scattering cross section (defined as a function of relative velocity g@ and angle q 0 of the vector g@ as a result of the collision), and dW 0 = sinq 0dq 0df is an element of solid angle about the vector g@ after collision. We note that the velocities va '@ and vb '@ in (5.3) are dependent on va@, vb@ and q 0.Expression (5.3) can be obtained in the following manner. Consider the number of collisions between particles
a in an element of volume d3 va with particles b in an element of volume d3 vb, as a result of which vector g is changed into the element of solid and dW 0. The number of these collisions is equal to
?
After collision, the particles considered are in the element of volume
d3 va' d3 vb' and have a relative velocity of g'@ = v'@ - v'. The number of reverse collisions is equal to
?
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Taking into account relations
d3 va d3 vb = d3 va' d3 vb', g = g', q 0 = q 0', dW 0 = dW 0' (see, for example [7]), and integrating over all scattering angles, (i.e., over all impact parameters) and over all particle b velocities, we can calculate the net change in the number of particles in an element of volume d3 va:
(5.4)
Dividing the result by
d3 va, we obtain the expression for the change in the number of particles a per unit volume of velocity space, i.e., the expression for the collision terms Iab in (5.3). Expression (2.4), which we used previously, is a special case of (5.3). Actually, if particles b can be assumed to be fixed, then g@ = va@ and vb@ = vb'@. In this case, by integrating over d3vb in (5.3) and by denoting ò fb(vb@ )d3vb = N, we obtain (2.4).We note that if the Maxwellian distribution functions
faM(va) and faM(vb@ ) with identical temperature (Ta = Tb) are substituted into Iab{fa(va@ ), fb(vb@ )}, the collision term naturally goes to zero, because ma va2 + mb vb2 = ma va' 2 + mb vb' 2, i.e., the collisions do not change the equilibrium energy distribution of the particles.If we write the distribution function
fe(v@ ) in the form of (2.1) and (2.5) and if we disregard the product of small values in the integrand, the expression for the collision term that describes electron-electron collisions assumes the form
(5.5)
Here q
' and q b' are the angles which indicate the directions of the velocity vectors v'@ and vb'@ after collision.We note that not only the direction but the value of the velocity
v changes during electron-electron collisions, which does not permit the use of the relaxation time approximation of §3. To find the distribution function in this case, it is necessary to solve the integral equation (2.3) with the right side of (5.2). Some methods for calculating the kinetic coefficients are considered below.The method of expansion by Sonine polynomials. To solve the integral equation (2.3), a method of solving the integral equation was employed in
[7] that includes expansion of the desired function c (v) into a series by Sonine polynomials S3/2 (n)(x):
(5.6)
where x = mev2/2kTe. Sonine polynomials are orthogonal over the range of values of x from 0 to ¥ with a weighting function x3/2exp(-x)
(5.7)
98
The zeroth and first Sonine polynomials are given by
S3(0)'2(x) = 1 and S3(1)'2(x) = 5/1 - x. Therefore, if the scattering mechanism leads to a relaxation time t p not dependent on energy, c (v) is expressed only by the zeroth and first Sonine polynomials (see formula (2.10)).In the general case, if the scattering mechanism is arbitrary, the desired function c
(v) is expanded into the series (5.6), but terminated in the term n = N. The expansion is substituted into equation (2.3) to obtain the coefficients a p @. For this, both sides of equation (2.3) are multiplied by S3(1)'2(x) (n = 0, 1, 2, ..., N) and are integrated over x. As a result, a system of N + 1 linear equations is obtained with respect to the expansion coefficients a p @, and the left hand sides of these equations, because of (5.7), include only coefficients a 0 and a 1.Thus, the problem of calculating the kinetic coefficients reduces to the solution of a system of equations for the values of a n, where, as follows from (2.1), (2.5), (3.1), (3.2), (5.6), and (5.7), the kinetic coefficients in the expressions for je and Se are dependent only on the expansion coefficients a 0 and a 1. The accuracy of finding the non-equilibrium distribution function and, consequently, the accuracy of calculating the kinetic coefficients is determined by the number of polynomials used in the expansion.*
The exact solution of the kinetic equation for the case where the relaxation time approximation is applicable (i.e., in the absence of electron-electron collisions) was compared [8] with the approximate solution of the same equation (obtained by the expansion of c (v) in Sonine polynomials) to evaluate the accuracy of this expansion method. The comparison showed that, in the case of electron-atom and electron-ion collisions (t pea ~ E1/2 and t pei ~ E1/2), use of the first two Sonine polynomials (N = 1) for calculation of mobility yields an error of only several percent (see curves 1 and 2 in Fig. 4.6)@. A much worse result is obtained, however, when the relaxation time decreases rapidly as the electron energy E increases (see curves 3 and 4 and II and III in Fig. 4.6).@ In this case c decreases rapidly as E increases, and c (E) is difficult to approximate by Sonine polynomials -- which are increasing functions of E.
The electrical conductivity of a completely ionized plasma in a magnetic field was calculated in [9] using an expansion by Sonine polynomials, where four polynomials (N = 3) were used for the expansion of the distribution function. Results from the calculation of the electron kinetic coefficients for a completely ionized plasma in a magnetic field, using a large number of polynomials (N = 5), are presented in [10]. The electron kinetic coefficients for a partially ionized plasma were calculated in [11, 12].
Fokker-Planck approximation. As indicated above, scattering at small angles, which lead to insignificant changes in the electron velocity, play the predominant role during electron-ion and electron-
____________________
*To calculate k e and Ke(T), it is necessary to take into account a greater number of expansion terms to achieve the same accuracy in view of the sign-changing of function c (v).
@The poor convergence of the approximations for electron scattering from Argon atoms is explained by the presence of a strong Ramsauer minimum in the electron scattering cross section at low energies, for this introduces a rapid decrease of t p with increase of E.
99
Fig. 4.6
electron collisions. In this case the motion of the electron in the velocity space can be regarded as diffusion. This approximation is called Fokker-Planck approximation.
In order to write the collision term (5.3) in Fokker-Planck approximation, consider the variation
< D F(va@ ) >ab of the arbitrary function F(va@ ), averaged by the particle velocities a, as a result of collision with particles b. This variation is equal to
(5.8)
Here
F(va@ ) and F(va'@ ) are the values of function F before and after collision, and the integration is carried out for the various types of collisions.Since the collisions involve only slight changes of velocity, the function
F(va@ ) can be expanded as a Taylor series
(5.9)
where D
va@ = va'@ - va@ is the change of velocity during collision, while the subscripts a and b denote the projections of the velocity to the corresponding coordinate axes. Substituting expansion (5.9) into (5.8) and integrating over d3va by parts, we obtain
(5.10)
where
(5.11)
(5.12)
100
The variation
< D F(va@ ) >ab resulting from collisions of particles a with particles b can also be written in a different form:
(5.13)
where
Iab is the collision term of the kinetic equation, which describes the change of the distribution function fa(va@ ) of particles a as a result of collision with particles b. Since (5.10) and (5.13) in the present approximation should be equal regardless of the specific form of function F(va), the integrands in (5.10) and (5.13) should also be equal, i.e.,
(5.14)
Relation (5.14) is the collision term in the Fokker-Planck approximation.
When using the Fokker-Planck approximation, we proceeded on the basis of collision term (5.3), which takes into account only binary collisions. However, the range of applicability of equation (5.14) is actually much broader. Formula (5.14) gives the variation of the distribution function in general, if this variation is caused by many small deflections. Expression (5.14), therefore, is valid for multiple Coulomb collisions and for describing the interaction of an electron with wave fields (if the change of momentum and energy during absorption and emission of field quanta are sufficiently small). However, in these cases, the values of
{D vaa }ab and {D vaa D vab }ab should be calculated for the specific type of electron interaction with the medium.We note that, in the Fokker-Planck approximation, the effect of small angle, multiple Coulomb collisions on the distribution function is similar to the effect of external fields, because in both cases the particle velocities vary in a continuous manner. This observation shows how a description of these collisions can be included in the kinetic equation (1.9), since the flow
ivc@ due to the effects of multiple Coulomb collisions can be added to the particle flow in velocity space, iv = f(v)F@/m, that results from an external force F@. In this way the collision term can be written as
(5.15)
Comparing (5.15) and (5.14), we obtain the expression for the particle flow due to the effects of Coulomb collisions:
(5.16)
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where
(5.17)
The particle flow
ivc@ is represented in (5.16) in the form of the sum of two terms. The term proportional to fa(va@ ), by analogy with particle flow iv@, is denoted as fa(va@ )Fc@ /ma. The value
(5.18)
is called the dynamical friction force. The last term in (5.16), which contains the derivatives of the velocity distribution function, is the diffusion flow in velocity space. The tensor
Dva b is called the diffusion-in-velocity coefficient.With binary Coulomb collisions, the values of
< D vaa >ab and < D vaa D vab >ab are expressed in the following manner:
(5.19)
(5.20)
where
mab = ma mb/( ma + mb ) is the reduced mass, ma and mb are the masses of colliding particles, Qp(g) is the momentum transfer cross section,* and d a b is the Kronecker delta (d a b = 1 for a = b and d a b = 0 for a ¹ b ).To derive (5.19), we substitute
v'@ - v@ = D v@ = (mab/ma)D g@ into (5.11) (see (3.1.8)) and obtain
(5.21)
Formula (5.21) expresses the change of the velocity,
The Fokker-Planck approximation for binary Coulomb collisions was used in
[6, 13] when calculating the electron kinetic coefficients for a completely ionized plasma. We note that although the Fokker-Planck approximation also simplifies the analysis of electron-electron collisions, nevertheless, the unknown function is still retained under the integral, because the values of < D va >ee and < D va D vb >ee are integrally dependent on the electron distribution function and, in particular, on the unknown component to the distribution function fe(1)(v@ ). Therefore, the solution of the integral-differential equation obtained in the Fokker-Planck approximation also requires numerical calculations, Sonine polynomial expansions being used in a number of cases (see, for example, [14]).____________________
*Cross section
Qp(g) is obtained from (3.2.10), if the particle velocity v and mass m in that equation are replaced by the relative velocity g and the reduced mass mab.
102
The nodal point method. In the relaxation time approximation, the kinetic coefficients are expressed as integrals of the non-equilibrium distribution function, of the type
(5.22)
where
x = E /kTe = mv2/2kTe and F(x) is some function (dependent on t p(x), w ct p(x), and the type of kinetic coefficient being considered).Integrals of type (5.22), with an infinite integration limit and a rapidly damped function under the integral, can be calculated not by the usual formulas (trapezoidal or Simpson formulas), but by using special Gaussian quadrature formulas, which have the form
(5.23)
where
xk(N) are the nodes of the quadrature formula and AR@(N) are the weight factors. The values of the nodes and weights are usually selected so that (5.23) yields a precise result if F(x) is a polynomial. Therefore, the formula with N nodes is equivalent to an approximation of the integrand with a polynomial of power 2N - 1. The accuracy of the quadrature formula (5.23) is high even for small values of N.It is obvious from (5.23) that the non-equilibrium distribution function need be calculated only at some (generally speaking, small) number of nodal points
xk in order to determine the kinetic coefficients. This advantage can be used in solving the kinetic equation when the relaxation time approximation is inapplicable, for example, when self-scattering of free electrons is important.In the Fokker-Planck approximation, the collision term for electron-electron collisions has the form
[6]
(5.24)
where
lnL is the Coulomb logarithm,
?
As can be seen from (5.24), the collision term in the Fokker-Planck form contains the derivatives and integrals of the desired function
D0(x). They can be expressed from values of D0(x) at nodal points by interpolating D0(x) in some manner, for example, by a Lagrangian interpolation. The
103
brace in (5.24), for this case, has the form at the
k-th nodal point
?
where m
ks(N) forms a general square matrix of rank N.If (5.24) is substituted into (5.2), and the result into (2.3), calculation of the non-equilibrium distribution function reduces to a system of linear equations for values of this function at the nodal points.
The matrix coefficients m
ks(N) with the number of nodal points N = 2, 3, 4, 5, and 6 were calculated in [15]. It was found, for a completely ionized plasma (1/t pea = 0), that the approximation with three nodal points leads to values of the kinetic coefficients which coincide with those obtained by a precise solution of the integral-differential equation. The latter solutions were presented above (see (5.1)).One of the advantages of the nodal point method is the increased accuracy in the presence of additional scattering mechanisms, electrons with heavy particles, whereas the term in (5.2) proportional to
1/t pea can be the main source of error in a solution of the integral equation by expansion in Sonine polynomials.The approximation for the electrical and thermal resistances in which the various contributions due to electron—atom and electron-ion scattering are simply added (Matthiessen’s rule) is frequently used in the calculation of kinetic coefficients for a partially ionized, multicomponent plasma. However, actually, the scattering mechanisms being considered have a different effect for electrons with different energies, so that the thermal and electric flows are always less than would be indicated by Matthiessen’s rule. Deviation from Matthiessen’s rule can be taken into account by introducing correction coefficients,
(5.25)
where m
ea, k ea, m ei, and k ei are values of kinetic coefficients in the limiting cases of a weakly ionized and of a completely ionized plasma.The correction coefficients
fm e, fk e and Ke(T), calculated by the nodal point method, for cases where t pea = const and lp = 1/NQpea = const, are depicted in Fig. 4.7 as a function of the ratio of the effective electron collision frequencies vea and vei with atoms and ions respectively. The effective collision frequencies vea and vei are essentially averaged inverse relaxation times and are calculated by the formulas
(5.26)
Here m
ea and m ei@ are the electron mobilities for electron scattering by atoms and ions, obtained by disregarding electron-electron collisions. The values of m ea and m ei@ are calculated by formulas (3.14) and (5.1), respectively, where g u = 1.The values of m
ea, Ke(T), and vea for the limiting case of a weakly
104
ionized, plasma are calculated by formulas (3.l4)-(3.l6). The values m
ei, Kei(T) and k ei for a completely ionized plasma are calculated by expressions (5.1).It is obvious from Fig. 4.7 that the maximum difference of
fm e
and fk e from unity is only » 25% at intermediate values of the ratio vei/vea. With regard to Ke(T), the dependence on vei/vea is very smooth, which allows an approximation of the results by simple formulas. We note also that, because of the large value of the Coulomb cross section, the transition from dominance by the one scattering mechanism to dominance by the other occurs in a weakly ionized plasma, that is, when ne « Na.
Fig. 4.7
6. Exchange of Energy and Momentum Between Electrons and the Heavy Components of a Plasma
Electrons lose their directed momentum and energy by collisions with heavy particles (atoms and ions). The rates of momentum and energy losses are determined by the relaxation times t
p and t E, respectively. With elastic collisions of electrons and heavy particles, t E/t p ~ M/m, where M is the mass of the heavy particle. As a result, the electrons in the plasma lose their directed velocity quite rapidly but lose their energy rather slowly. This leads to the fact that the electron distribution function has a low anisotropy in velocity space, whereas the electron energy distribution in a number of cases may differ considerably from the equilibrium distribution.In a TIC plasma, it is possible to establish a Maxwellian energy distribution as a result of the intensive electron-electron collisions among the bulk of the electrons. However, the average energy and temperature
Te of the electrons usually differs appreciably from the average energy and temperature T of the heavy particles, because of the weak exchange of energy between the electrons and heavy particles. We now turn to the calculation of the momentum and energy imparted by the electrons to the heavy particles during collisions.Change of the electron momentum during collisions with atoms and ions. The forces acting on the electrons in the plasma. Since electron collisions with atoms and ions lead to change of the electron momentum, the electrons of the plasma, as a result of these collisions,
105
are acted on by the force
Re@, equal to
(6.1)
The values of
Rea@ < D pe@ >ea and Rei@ < D pe@ >ei are the force components of Re@, determined by the change of the electron momentum during collisions with atoms and with ions. They are a function of the momentum relaxation times t pea and t pei, respectively.When the Maxwellian distribution function
feM(v) is substituted into (6.1), the force Re@ goes to zero. Therefore, only the non-equilibrium component fe(1)(v@ ) to the distribution function should be substituted into the integrals of (6.1)It is possible to show that, with low electron drift velocity
(vde « ve), and in the absence of a magnetic field, the effect of force Re is equalized by the force - eneE@ - gradpe associated with the electric field and the pressure gradient, i.e.,
(6.2)
By comparing (3.3) and (6.2), we find the following expression for force
Re@:*
(6.3)
It is obvious that force
Re consists of two components: the friction force Re(m )@ = - je@ /m e, caused by a relative velocity between the plasma components, and the so-called thermal force Re(T)@ = -Ke(T)nekgradTe, generated by the presence of the electron temperature gradient. If the relaxation time t p is not dependent on energy, then the thermal-diffusion ratio Ke(T), and therefore, the thermal force, approaches zero. In this case, the momentum transport of the electrons due to the heavy component is proportional to current je@, which can also be seen directly on the basis of expression (6.1).The occurrence of the thermal force is related to the dependence of relaxation time t
p on electron energy E. As already indicated in §3, at je@ = 0 and in the presence of an electron temperature gradient, two mutually compensating counter flows of electrons pass through the plasma. If t p increases as E increases (Ke(T) > 0), the flow of slower electrons moving in the direction of the temperature increase loses greater momentum during collisions than a flow of faster electrons moving in the opposite direction. Therefore, the resulting force acting on the electrons is directed in the direction opposite to the flow of slow electrons, i.e., in the direction of the decrease of electron temperature. On the other hand, if t p decreases as E increases (Ke(T) < 0), the thermal force is directed toward the increase of electron temperature.___________________
*Expression (6.3) can be obtained in a more accurate way if both sides of (2.3) at w
c = 0 are multiplied by mev@ and integrated over velocities. In this case, the right side of (2.3) should be represented in the form (5.2) (where ò Iee{fe(v@ )}mv@ d3v = 0, because electron-electron collisions do not alter the total momentum of the electron subsystem), and - eneE@ - gradpe in the left side of (2.3) must be expressed in je@ and grad Te by using (3.3).
106
Energy transfer from electrons to atoms and ions during collisions. The energy transfer from electrons to the heavy component of the plasma may occur either because of electron-atom or because of electron-ion collisions, the relative importance of the two depending on the degree of ionization of the plasma. In either case, individual collisions are accompanied by insignificant changes in the electron energy, which allows a description of the electron shift in energy space using the Fokker-Planck approximation.
In general, the energy transferred from particles
a (electrons) to particles b (ions or atoms) during collisions can be expressed as
(6.4)
The value of D
Sab is assumed to be positive if energy passes from particles a to particles b.If the heavy particles have a Maxwellian distribution, only the spherically symmetrical part of the electron distribution function
fa(0)(va) contributes to the integral (6.4). Therefore, the Fokker-Planck equation for a spherically symmetric electron distribution function must be formulated in order to calculate D Sab In this case, the particle flow ivc@ in velocity space is directed along the electron velocity va@.To obtain
ivc@, consider first electron-ion collisions. In calculating the dynamic friction force Fc@ by formulas (5.18)-(5.20), disregard for now the ion velocities vb@ compared to va@ in (5.19) and (5.20). Then, since we assume g = va, we obtain
(6.5)
(6.6)
where
Nb = ò fb(vb@ )d3vb is the ion density. By substituting (6.5) and (6.6) into (5.18), and by using the definition of the reduced mass (3.1.4), we obtain
(6.7)
The diffusion tensor
Dva b , given by formula (5.17), can be calculated in the coordinate system with the z-axis parallel to va@. Tensor Dva b is diagonal if the particle distribution over velocities in this coordinate system is spherically symmetric. By denoting the tensor component Dvzz by Dv| | , we obtain from (5.16)
(6.8)
In the approximation used here (disregarding the velocities
vb of slow particles), the tensor component Dv| | , as can be seen from (5.17) and (5.20), is equal to zero.* Therefore, when calculating Dv| | , it is necessary to retain the terms of order vb/va in (5.20). However, if the_____________
*This result is related to the fact that electrons do not acquire energy during scattering from fixed centers. They only lose energy-this process is described by the dynamical frictional force. Diffusion in velocity space occurs only in the direction perpendicular to
va@, The corresponding diagonal components Dvxx = Dvyy are distinct from zero.
107
particles
b have a Maxwellian distribution (characterized by temperature Tb), the diffusion coefficient Dv (we shall now omit the subscript | | ), can be found by a simpler method, namely from the condition that ivc@ = 0 when particles a have a Maxwellian distribution with temperature Ta = Tb. In this case, thermodynamic equilibrium occurs between particles a and b. Then, by assuming fd(0)(va) = fM(va) and ivc = 0, we obtain
(6.9)
Substituting (6.9) into (6.8), using (6.7), and taking into account (3.l.14), we find the following expression for the particle flow in velocity space:
(6.10)
According to (5.15), the collision term can now be written in the form
(6.11)
Expression (6.10) and (6.11) can be used not only for electron-ion collisions, but also for electron—atom collisions, if
Qp(va) is understood as the momentum transfer cross section corresponding to these collisions. Note that only the condition va » vb was used when deriving expression (6.10). The condition of the smallness of the mass ma compared to mass mb was not used. Therefore, these derived expressions can also be used when considering fast electron collisions with slow electrons with a Maxwellian distribution, entering into these expressions ma = mb = m and Tb = Te (see §5, Chapter 5).To calculate the energy lost by the electrons during collisions with heavy particles, substitute (6.10) and (6.11) into (6.4). Assuming that
fa(va) = fe(0)(v), ma = m, Tb = T (the temperature of the heavy component of the plasma), and d3 v = 4p v2dv, we obtain
(6.12)
where the subscript
b corresponds to atoms or ions.If the electrons have a Maxwellian distribution and
fe(0)(v) = feM(v), then, by integrating (6.12) by parts, we obtain
(6.13)
where the symbol
<...> denotes averaging over the distribution function, and ne = 0ò ¥ 4 p v2feM(v)dv is the electron density. The energy relaxation time t E in (6.13) can be expressed in terms of the momentum relaxation time t p using the following relation which results from (3.1.13) and (3.1.14)
108
(6.14)
By disregarding the electron mass
m compared to the atomic mass, we obtain the following expression from (6.13) and (6.14) for electron-atom collisions:
(6.15)
where
Ma = mb is the atomic mass.The effective energy exchange time t
Qea is so determined that if the relaxation time t p is not dependent on electron energy, then t Qea » t p. If t p and the mean free path (lp = vt p) are proportional to the r-th power of energy (3.13), then t Qea = 3l0/2ve@ G (3 - r). In particular, if the mean free path is constant (r = 0), t Qea = 3l0/4ve@.The result for electron-ion collisions can be described in the same way. For this case, from (6.13), (6.14), (3.1.13), and (3.2.10), disregarding
m compared to the ion mass Mi, we obtain
(6.16)
where
(6.17)
The variable
ni is the ion density and Mi is the ion mass (ni = Nb,MI = mb)
.As can be seen from (6.15) and (6.16), the relaxation time of the electron temperature
Te to the temperature T of the heavy particles is of the order (M/m)t p, i.e., much greater than the momentum relaxation time t p. An exception to this occurs for molecular gases in which vibrational and rotational levels can be excited. The relaxation time of the electron temperature in these gases is several orders less.The electron distribution function in a strong electric field. In the above discussion of kinetic phenomena, the electric field and density gradient were assumed to be everywhere small. Under these conditions the electron distribution function hardly differed from the Maxwellian distribution. Consider now the case where the electron distribution function differs strongly from the Maxwellian distribution. This may occur in the presence of strong electric fields or of large density gradients. Large density gradients are considered primarily in the discussion of electrode sheaths (see §
6, Chapter 6). A homogeneous gas located in a strong electric field will be considered in this section.It is interesting to note that even in a strong electric field the electron distribution function is characterized by weak anisotropy in velocity space. The energy acquired by the electron from the field per unit time is D
EE = vdeeE » (et pE/m)eE, and the energy imparted to the heavy component of the plasma during collisions is D Ec » (mv2/t p)m/M. In the steady state we have D EE = D Ec and accordingly, v » (et pE/m)Ö M/m@
109
» vdeÖ M/m@ >> vde
. * Thus, the directed electron velocity vde in a homogeneous plasma should be considerably less than the random velocity v, even in a strong electric field.Weak anisotropy of the electron distribution function
fe(v@ ) in a strong field leads to the fact that fe(v@ ) may be represented in the form
(6.18)
where
fe(0)(v) is the isotropic part of the distribution function and fe1(v) cosq is the small anisotropic component, which (as in the case of a weak electric field) is represented in the form of the product of cosq and the function fe1. The latter is dependent only on the velocity modulus (compare (2.1)). The difference from the case of a weak field is in the fact that fe(0)(v) now no longer coincides with the Maxwellian distribution function feM(v), so that, along with the equation for calculation of fe1(v), it is necessary to formulate the equation to find fe(0)(v).The equations for the calculation of
fe(0)(v) and fe1(v) can be obtained by the following method [16]. First we integrate the kinetic equation (1.9) term wise over dW . Using (6.18) and the relation
?
and having divided the result obtained above by
4p , we obtain
(6.19)
where
I0 = 1/4p ò I{ fe(v@ )}dW . In like manner, having multiplied both sides of (1.9) by cosq , having integrated over W , and having divided the result by 4p /3, we obtain
(6.20)
where
I1 = 3/4p ò I{ fe(v@ )}cosq dW .The electron distribution function, for a homogenous plasma located in a steady electric field of arbitrary strength,
@ is calculated from equations (6.19) and (6.20). The values of I0 and I1 characterize the rate of change due to collisions of the isotropic and anisotropy parts, respectively, of the distribution function. To an order of magnitude, I0 » fe(0)(v)/t E and I1 » fe1(v)/t p, i.e., the relaxation rate_______________
*This result was obtained with the assumption that the mean electron energy greatly exceeds the mean energy of the heavy particles
kT. If this is not true and v » Ö kT/m@, then the average energy transferable during each collision decreases compared to the value (mv2/t p)m/M, and accordingly, v may exceed (et pM/m)Ö M/m@.@
Equations (6.19) and (6.20) are easily generalized for the case of an inhomogeneous and transient plasma. However, in this case, variation of the distribution function in time and space should be sufficiently slow [17].
110
of the isotropic part of the distribution function to the Maxwellian function
feM(v) is determined by the energy relaxation time t E while the relaxation rate of the anisotropy part of the distribution function to a spherically symmetric distribution is determined by the momentum relaxation time t p.Consider now in which cases the application of an electric field can significantly distort the isotropic part of the distribution function
fe(0)(v) from the Maxwellian function. Having calculated fe1(v) from (6.20) and having substituted it into (6.19), we find that the ratio of the left side of (6.19) to the right side (to an order of magnitude) is determined by the parameter b = e2E2t pt E/m2v2.If b
« 1, then the left side of (6.19) can be set equal to zero in the first approximation. Then fe(0)(v) is calculated from the equation I0 {fe(0)(v)} = 0. This equation is satisfied if fe(0)(v) is a Maxwellian distribution function with a temperature equal to the temperature T of the heavy particles. In this case, we have mv2 » kT and b » e2E2t pt E/mkT. Thus, fe(0)(v) » feM(v) and Te » T, if e2E2t pt E/mkT « 1. This is for the case of a weak electric field.Consider the opposite case, of a strong field, where
e2E2t pt E/mkT » 1. In this case, the average electron energy considerably exceeds kT, and as was indicated above, v » (et pE/m)Ö M/m@, since b » (t E/t p)m/M. If the plasma is very weakly ionized, so that not only the momentum relaxation but the energy relaxation as well are provided by electron-atom collisions, then t E/t p » M/m and b » 1. In this case, the isotropic part of the distribution function may differ strongly from a Maxwellian distribution.A different situation arises if the degree of ionization of the plasma increases, so that energy relaxation is provided by electron-electron collisions, i.e., when t
Eee « t Eea » (M/m) t pea. Under these conditions, b » (t Eee/t Eea)m/M « 1. The condition b « 1 is fulfilled to an even greater extent if the degree of ionization of the plasma is so great that momentum relaxation is provided by electron-ion rather than by electron-atom collisions. In this case t Eee » t pei, and therefore, b » m/M. Under these conditions, the electron distribution function relaxes rapidly to a Maxwellian distribution as a result of electron-electron collisions. An increase of field intensity now leads to an increase of electron temperature Te compared to the heavy particle temperature T,* rather than to deviation of the isotropic part of the distribution function from a Maxwellian distribution.Consider now in more detail the case of a weakly ionized plasma, where the energy relaxation is provided by electron-atom collisions. In this case,
I0 is expressed by formulas (6.10) and (6.11), in which it is necessary to set t Eab(v) = t Eea(v) and I1 = - fe1(v)/t pea(v). Having obtained fe1(v) from (6.20) and having substituted it into (6.19), we find the equation for the distribution fe(0)(v):
(6.21)
_______________
*The electron temperature is calculated from the condition D
Seb = jeE(b = a, where D Seb is the energy transferred from the electrons to the heavy particles (see (6.15) and (6.16)), and je is the electron current.
111
The expression in brackets in (6.21) is the total particle flow
iov in velocity space (with the opposite sign): the particle flow due to the effects of the electric field is added to the particle flow due to the effects of collisions ivc. The essence of formula (6.21) is that the divergence of the total particle flow in velocity space is zero. Integrating (6.21), we obtain v2iov = const. Assuming in this last expression that v = 0, we find that the integration constant is zero. But since the expression is true in general, we find that the flow itself, iov, is equal to zero.Setting the expression in the brackets of (6.21) equal to zero and integrating the differential equation obtained, we obtain further
(6.22)
The integration constant
C is calculated by the normalization condition (1.1) and is therefore a function of the electron density ne. In a weak electric field, by assuming E = 0 in (6.22), we obtain the Maxwellian distribution in which the electron temperature is equal to the atom temperature T. In a strong electric field, on the other hand, @ can be disregarded in the exponent. And the form of the distribution function fe(0)(v) is determined by the nature of the function t pea(v).By assuming a constant mean free path
(l = vt pea(v) = const), andby assuming t
Eea(v) = (M/2m) t pea(v), we obtain from (6.22) the well known Druyvesteyn distribution [18]
(6.23)
which decreases much more rapidly at high velocities than the Maxwellian distribution .
For
fe1(v), we obtain from
(6.24)
Calculating the average electron energy according to (1.3), we find
(6.25)
and calculating current
je according to (3.1), we obtain the electron mobility
(6.26)
Expressions (6.25) and (6.26) are for strong fields, where
e2E2t pt E/mkT » 1.
7. The Kinetic Coefficients for Ions in a Weakly Ionized Plasma
The expression for ion flow in a weakly ionized plasma has a form similar to (3.3) and differs from this only by the presence of the
112
force
Rie@ with which the electron flow acts on the ions as a result of electron-ion collisions. The effect of force Rie@ on the ions is similar to the effect of external forces. Therefore, force Rie@ is added to force eniE@, with which the electric field acts on the ions. It is obvious that Rie@ = -Rei@. The force Rei@ can be accounted for in the same way that Coulomb collisions are treated in the calculation of m e and Ke(T).The value of
Rei@ can be calculated easily if the degree of ionization of the plasma is sufficient that Coulomb collisions predominate over electron-atom collisions (u ei@ » u ea@). In this case, Rei@ is calculated by formula (6.3), into which the values of mobility Pe and of the thermal-diffusion ratio Ke(T) that correspond to a completely ionized plasma (calculated by formulas (5.1)) must be substituted.If the scattering mechanism is mixed, when u
ei@ » u ea@, the force Rie@ may no longer be expressed so simply by the electron kinetic coefficients. In this case, Rei@ may be written in the form
(7.1)
where
g1 and g2 are the coefficients which are dependent on the ratio u ei@/u ea@. Expression (7.1) follows from the fact that the non-equilibrium component fe(1)(v) in the electron distribution function is proportional to the gradients pe and Te and to the electric field E@.The dependence of
g1 and g2 on the ratio of the effective collision frequencies u ei@/u ea@ is shown in Fig. 4.8 [12]. In the limiting case of a weakly ionized plasma, when u ei@/u ea@ ® 0, force Rei@ does not contribute to Re and the coefficients g1 and g2 approach zero. In the opposite case, when u ei@/u ea@ ® ¥ , Re@ = Rei@. Then, by comparing (3.3) and (6.3), we find g1 = 1 and g2 = 0.With regard to the force of electron—ion friction, the expression for the ion current density assumes the following form (compare (3.3)):
(7.2)
Therefore, by taking into account (7.1), we obtain
(7.3)
The quasi-neutrality of the plasma is taken into account in (7.3), and the charged particle density is denoted by
n(ne = ni = n).We note that the thermal-diffusion ratio
Ki(T) for ions is small (see [12]), where Ki(T) ® 0 as the frequency of ion-ion collisions increases, due to the fact that during intensive ion-ion collisions the ion distribution function begins to approach a Maxwellian distribution fiM(ï v@ - vdi@ ï ) shifted by the value vdi@ = - ji@ /eni of the ion drift velocity (see page 95).Expressions (7.2) and (7.3) are appropriate for weak gradients of potential, density, and temperature, when the ion distribution function does not differ significantly from the Maxwellian distribution function (see §
2). However, ion mobility in moderate and strong electric fields will also be of subsequent interest (see §2, Chapter 6).
113
We note that the calculation of ion mobility in a strong electric field, generally, is a very complicated problem. A strong field not only significantly alters the ion energy distribution, but also leads to a strong anisotropy of the ion distribution function in velocity space, which does not occur in the case of the electron distribution function. Therefore, even in the case of a very weakly ionized plasma, when ion-ion and electron-ion collisions do not affect ion motion, ion mobility in an electric field of arbitrary strength has been calculated only for some, quite specific, scattering mechanisms. Two distinct cases are considered below - ion motion in a gas consisting of molecules of any other material, and ion motion in their own gas.
Fig. 4.8
Ion mobility in a foreign gas. Ion interaction with foreign neutral molecules reduces primarily to the polarization of these molecules and to the attraction of the ion by the polarized molecules. The force of ion attraction to the polarized molecule is equal to
[19]
(7.4)
where a is the polarizability of the molecule and
r is the distance between the molecule and the ion. The interaction (7.4), for which the force is inversely proportional to the fifth power of the distance, has the remarkable property that the product of the relative velocity g and cross section s (g, q 0) is not dependent on g. Because of this, the momentum transferred to the molecules during ion collisions, < D pi@ > im, can be calculated without finding the ion distribution function.We may use expression (5.8) to calculate <
D pi@ > im, and to do so, we turn to the center of mass system for the ion and molecule. The change of ion momentum during collision with a molecule is then expressed as D pi@ = pI'@ - pim@ = mi(g'@ - g@), where mim = MiMm/(MI + Mm) is the reduced mass, Mi is the ion mass and Mm is the mass of the molecule (see (3.1.9)). Substituting D pi@ into (5.8), we find
(7.5)
where
fm(vm@ ) and fi(v@ ) are the molecule and ion velocity distributionfunctions, respectively, and
Rim@ is the frictional force acting on the ions as a result of collisions with the molecules.If the value of
1/t pim = gNmò (1 - cosq 0)s (g, q 0)dW 0 is not dependent on the relative velocity of the colliding particles, then, by substituting g@ = v@ - vm@ into (7.5), we obtain
(7.6)
114
where
Nm = ò fm(vm@ )d3vm is the molecular density. Performing the integration over ion and molecule velocities in (7.6), we find
(7.7)
where
vdi@ and vdm@ are the average drift velocities of the ions and molecules, respectively. Since the frictional force Rim@ in a homogenous electric field in steady state is equalized by the force of the electric field eniE@, it follows from (7.7) that the relative ion velocity is equal to
(7.8)
where
(7.9)
is ion mobility. We have already previously obtained a similar expression for electron mobility in the approximation of constant relaxation time (see (3.8)).
We note that the area of validity of expressions (3.8) and (7.9) is broader than that of the remaining results obtained in §§
2 and 3 of this chapter or in equation (7.3): expressions (3.8) and (7.9) are valid for mobility (given a constant relaxation time) not just for a weak electric field but for an arbitrary electric field, because formula (7.8), as can be seen from its derivation, is valid for any form of the velocity distribution function.Formula (7.4) describes the ion interaction with atoms and molecules at large distances. At small distances, when the exchange forces become important, it is no longer valid. For ion collision with atoms and molecules, one can consider an approximate model of elastic spheres. In this model, ion mobility is given by the following expression
[7]:
(7.10)
where
Qpim = p (ri + rm)2 (ri and rm are the radii of the ion and molecule).Langevin developed theories of ion mobility in a weak electric field by treating both the polarization interaction and ion-molecule collisions as collisions between elastic spheres
[19 - 21].Ion mobility in their own gas. When positive ions move in their own gas, the main process of ion interaction with the atoms is resonance charge exchange - the transfer of the charge from the ion to the atom. The particle velocities are exchanged after resonance charge exchange. This simplifies the calculation of ion mobility. The collision term of ions with atoms for charge exchange is written in the form
(7.11)
where
v@ and va@ are the ion and atomic velocities prior to collision and s (g, q 0) is the differential cross section of the charge exchange. Expression (7.11) follows from (5.3), if we take into account that the atom and ion after collision seem to have exchanged velocities, i.e., v'@ = va@ and va'@ = v@.
115
In the simplest case of constant relaxation time, when
g ò s (g, q 0)dW 0 is not dependent on the relative velocity of the colliding particles
(7.12)
where
ni and Na are the densities of the ions and atoms and t ia is the time of the free path:
(7.13)
Here
Qia(g) = ò s (g, q 0)dW 0 is the total cross section for charge exchange. If the atoms have a Maxwellian distribution, then (ni/Na)fa(v) = fiM(v), where fiM(v) is the Maxwellian distribution function for ions at a temperature equal to the gas temperature T. In this case, the kinetic equation for ions is written in a form similar to (1.9) and (2.8):
(7.14)
However, unlike the case considered in §
2, the non-equilibrium part of the distribution function fi(v@ ) - fiM(v) may not be quite as small.Multiplying both sides of (7.14) by
ev@ and integrating over d3v, we obtain the expression for current ji@ = - eii' = - em iniE@, where m I = et ia/Mi is the ion mobility. Thus, the approximation of a constant relaxation time permits a very simple calculation of the ion mobility in an electric field of arbitrary intensity.
Fig. 4.8
However, the approximation of a constant relaxation time presupposes the specific dependence of the charge-exchange cross section on relative velocity:
Qia(g) ~ g -1. Actually, the cross section @ is weakly dependent on g, so that the approximation of a constant cross section Qia, and accordingly, of a constant mean free path li = 1/QiaNa is more accurate. In this case, the solution of the kinetic equation with the collision term (7.11) is very complicated. Results from a numerical solution of the kinetic equation for ions in a homogeneous electric field, obtained in [22], are presented below.*The dependence of the ion drift velocity
vdi@ on the electric field E@ is presented in Fig. 14.9. Here the drift velocity and the field are given in dimensionless units: z@ = vdi/(2kT/Mi)1/2 and g = p eEli/4kT._____________
*When calculating ion mobility, it is convenient to turn from the integral-differential kinetic equation to the integral equation, which will be formulated in §
2 of Chapter 6 for the case of a strong field (in this regard also see [23]).
116
The dashed lines denote the limiting values of ion drift velocity in weak and strong electric fields. The points and the solid line plotted through them are the results of calculations with intermediate values for the field intensity. For weak fields
(g « 1), ion mobility with charge exchange was calculated independently by an expansion of the non-equilibrium component to the distribution function into a series of Sonine polynomials [24] and was found to be equal to
(7.15)
For the case of strong fields
(g » 1), ion mobility in the approximation of a constant mean free path, as indicated below (see §2, Chapter 6), is equal to m i = Ö 2eli/p MiE@ (see (6.2.11)).
117
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