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Collisions

If Λ \Lambda is large, then small-angle scattering dominates.

ν=n2πϵ02e4m2v03lnAnT3/2m1/2 \nu = \frac{n}{2 \pi \epsilon_0 ^2} \frac{ e^4}{m^2 v_0 ^3} \ln \Alpha \propto \frac{n}{T^{3/2} m^{1/2}}

Paschen curve for breakdown

Say we have two large parallel plates

Figure 11.2

Figure 11.3

You can stay on the g=1 curve by putting a large resistor on your power supply, so it's always running like it's about to break down. Neutral-dominated plasma (neutral resistance).

To the left of the Paschen minimum, the spacing is less than the mean free path. There are surface losses. Electron loss to wall.

To the right of the Paschen minimum, there's a fairly linear region with

  • Local losses
  • There is a certain ΔV \Delta V required between collisions that must be large enough to generate another electron before the electron is lost (l l = spacing between the plates, lmfp l_{mfp} = mean free path

    ΔV=Elmfp=Vllmfplmfp1n1p \Delta V = E l_{mfp} = \frac{V}{l} l_{mfp} \qquad l_{mfp} \propto \frac{1}{n} \propto \frac{1}{p}

    If you solve,

    ΔV=Vlpconst. \Delta V = \frac{V}{l p} \cdot \text{const.}

    V=pl(ΔVconst.)=plconst. V = p l \left( \frac{\Delta V}{\text{const.}} \right) = p l \cdot \text{const.}

g=1 g = 1 is used for voltage regulation.

Definition of Plasma

Some basic criteria for plasma are

LλD (neutral plasma)  L \gg \lambda_D \qquad \text{ (neutral plasma) }

Λ1(ωpeνei \Lambda \gg 1 \qquad (\omega_{pe} \gg \nu_{ei}

νen<ωpe(if neutrals) \nu_{en} < \omega_{pe} \quad \text{(if neutrals)}

The collision frequencies have the following meanings:

  • νei \nu_{ei} - Electron momentum loss rate on ions. Used in resistivity.
  • νee \nu_{ee} Electron energy exchange rate with electrons. In other words, if you do something to the electrons this is how long it will take to get back to Maxwellian. Same order as νei \nu_{ei}
  • νii \nu_{ii} Ion energy exchange rate with ions
  • νie \nu_{ie} Electron energy exchange rate between electrons and ions. It's about the same as ions slowing down in electrons: memiνee \approx \frac{m_e}{m_i} \nu_{ee} . For fusion to work, need confinement times longer than this time.

Electrical Resistivity

Place a plasma of density $n$ in an electric field (generated by voltage difference V). Electrons accelerate in one direction and ions in the other

Δp=FΔt \Delta p = F \cdot \Delta t

Electrons and ions both get accelerated then collide and both stop since they had equal and opposite momentum

Δw=Fdistance \Delta w = F \cdot \text{distance}

The energy transfer will be much higher for the electrons because of their lower mass. So the electrons carry the current and receive ohmic heating for the resistive part of impedance

mivi=mevevevi \langle m_i v_i \rangle = - \langle m_e v_e \rangle \rightarrow v_e \gg v_i

The approx current is given by the drift velocity vd v_d by disregarding the velocity of the ions:

j=neve+nevineve=nevd j = - n e \langle v_e \rangle + n e \langle v_i \rangle \approx - n e \langle v_e \rangle = |n e v_d|

Identifying the resistivity with Ohm's law

E=ηj E = \eta j

The force on the electrons is the rate at which momentum is lost by the electrons, which is the drift velocity times the electron-ion collision rate:

Felec=Ee=mvdνei=momentum loss rate F_{elec} = E e = m v_d \nu_{ei} = \text{momentum loss rate}

ηj=E=meνeinevdne2 \rightarrow \eta j = E = \frac{m_e \nu_{ei} n e v_d}{n e^2}

η=meνeine2 \rightarrow \eta = \frac{m_e \nu_{ei}}{n e^2}

Recall the collision frequency

νei=n2πe4ϵ02m2v02lnΛ \nu_{ei} = \frac{n}{2 \pi} \frac{e^4}{\epsilon_0 ^2 m^2 v_0 ^2} \ln \Lambda

η=mene2n2πϵ02Zeffme2e4v03lnΛ \eta = \frac{m_e}{n e^2} \frac{n}{2 \pi \epsilon_0 ^2} \frac{Z_{eff}}{m_e ^2} \frac{e^4}{v^3 _0} \ln \Lambda

The velocity is given by the electron thermal speed

v03(Teme)3/2 v_0 ^3 \propto \left( \frac{ T_e}{m_e} \right) ^{3/2}

The densities cancel and we can plug in some values

η=5105lnΛTe3/2(Hydrogen) \eta = 5 \cdot 10^{-5} \frac{\ln \Lambda}{T_e ^{3/2}} \qquad \text{(Hydrogen)}

Magnetic Decay Time

The magnetic decay time for parallel current. For current parallel to the magnetic field, the curl of B is just some multiple λ \lambda of B:

×B=λB=μ0j=μ0EηE=ληBμ0 \curl B = \lambda B = \mu_0 j = \mu_0 \frac{E}{\eta} \rightarrow E = \frac{\lambda \eta B}{\mu_0}

×E=Bt \curl E = - \pdv{B}{t}

×ηλμ0B=Bt \rightarrow \curl \frac{\eta \lambda}{\mu_0 } B = - \pdv{B}{t}

This tells you the rate of decay of the magnetic field when you have helicity. The relevant timescale of the decay is

ηλ2Bμ0=dBdtτ=μ0ηλ2 \frac{\eta \lambda^2 B}{\mu_0} = - \dv{B}{t} \rightarrow \tau = \frac{\mu_0}{\eta \lambda^2}

Thermal Conductivity

Consider a region of space where we have a hot side and a cold side. There is a heat flux Q Q flowing from the hot to the cold side

Q=powerarea Q = \frac{\text{power}}{\text{area}}

The thermal conductivity κ \kappa is defined by

QκTz Q \equiv - \kappa \pdv{T}{z}

If the energy/particle going up / going down is ε \varepsilon

Q=ε0ndownvdownε+nupvup Q = \varepsilon _0 n_{down} v_{down} - \varepsilon _+ n_{up} v_{up}

For mass conservation we must have

ndownvdown=nupvup=nv n_{down} v_{down} = n_{up} v_{up} = nv

Q=ε0nvε+nv Q = \varepsilon _0 n v - \varepsilon_+ nv

If we're calculating the heat flux at some position z z and the mean free path is l l then particles come from about a mean free path distance. The energy dependence on z z is given as ε(z) \varepsilon(z)

Qnv[ε(zl)ε(z+l)] Q \approx n v \left[ \varepsilon (z - l) - \varepsilon(z + l) \right]

Qnv[(ε(z)lεz)(ε(z)+lεz)] \rightarrow Q \approx n v \left[ \left(\varepsilon (z) - l \pdv{\varepsilon}{z}\right) - \left(\varepsilon(z) + l \pdv{\varepsilon}{z}\right) \right]

nvlεz \approx - n v l \pdv{\varepsilon}{z}

The Maxwell-Boltzmann energy of the particles is

ε(z)=kT(z) \varepsilon (z) = k T(z)

QnvlkTz Q \approx - n v l k \pdv{T}{z}

κ=knvlmfp \kappa = knv l_{mfp}

Now we plug in the mean free path, assuming lmfpz0 l_{mfp} \ll z_0 (where z0= z_0 = plasma size.

lmfp=vtc=vν(kT)1/2T2/3m1/2m1/2nlnΛ l_{mfp} = v t_c = \frac{v}{\nu} \approx \frac{(k T)^{1/2} T^{2/3} m^{1/2}}{m^{1/2} n \ln \Lambda}

κT5/2m1/2lnΛT5/2m1/2 \rightarrow \kappa \sim \frac{T^{5/2}}{m^{1/2} \ln \Lambda} \sim \frac{T^{5/2}}{m^{1/2}}

If there is no magnetic field (or we're looking parallel to the field) then

κT5/2m1/2 \kappa \propto \frac{ T^{5/2}}{m^{1/2}}

There's a thing called the conductivity of the Lorentz gas (ions are infinitely massive)

κlorentz4.671012T5/2ZlnΛ \kappa_{lorentz} \approx 4.67 \cdot 10^{-12} \frac{T^{5/2}}{Z \ln \Lambda}

κZ=14.41013T5/2ZlnΛ \kappa_{Z=1} \approx 4.4 \cdot 10^{-13} \frac{T^{5/2}}{Z \ln \Lambda}

What happens when we add a magnetic field? B=B0 B = B_0

lmfprg l_{mfp} \rightarrow r_g

rg r_g = radius of gyration = vω \frac{v}{\omega}

rg=vωlmfp=vτcτc=1ν r_g = \frac{v}{\omega} \qquad l_{mfp} = v \tau_c \qquad \tau_c = \frac{1}{\nu}

rglmfp=vω1vτc=1ωτcκ \frac{r_g}{l_{mfp}} = \frac{v}{\omega} \frac{1}{v \tau_c} = \frac{1}{\omega \tau_c}\rightarrow \kappa

where κ \kappa is reduced by a factor 1ωτc \frac{1}{\omega \tau_c} compared to the non-magnetized plasma. The energy is now transmitted over a shorter distance, but it also has a lower fluence. The particles move a distance rg r_g over every time τc \tau_c , so the transport velocity is reduced

vrgτc reduced by rgvτc=1ωτ(v=ωrg) v \rightarrow \frac{r_g}{\tau _c} \rightarrow \text{ reduced by } \frac{r_g}{v \tau_c} = \frac{1}{\omega \tau} \quad (v = \omega r_g)

That's an additional reduction by 1ωτ \frac{1}{\omega \tau} , so

κBκ0(1ωτ)2 \kappa_B \approx \kappa_0 \left( \frac{1}{\omega \tau}\right) ^2

What is the mass dependence

κB1m1/2(mm1/2)2=m1/2 \kappa_B \rightarrow \frac{1}{m^{1/2}} \left( \frac{m}{m^{1/2}} \right) ^2 = m^{1/2}

In the cross-field direction, ions dominate the cross field thermal conduction

κκ,e(1ωceτee)2(mime)1/2 \kappa _\perp \approx \kappa_{\parallel, e} \left( \frac{1}{\omega_{ce} \tau_{ee}} \right)^2 \left( \frac{m_i }{m_e} \right) ^{1/2}

or

κ,i(1ωciτii)m1/2T5/2(nBT3/2)2m1/2n2B2T1/2 \approx \kappa_{\parallel, i} \left( \frac{1}{\omega_{ci} \tau_{ii}} \right) \propto m^{1/2} T^{5/2} \left( \frac{n}{B T^{3/2}} \right) ^2 \propto \frac{m^{1/2} n^2}{B^2 T^{1/2}}

To get real numbers, use Spitzer

κ=1.61040Ai1/2n2lnΛT1/2B2 \kappa_\perp = 1.6 \cdot 10^{-40} \frac{A_i ^{1/2} n^2 \ln \Lambda}{T^{1/2} B^2}

where T T is in eV eV , B B is in Tesla, n n is in m3 m^{-3} , Z Z is the atomic charge, and Ai A_i is the atomic mass number

η=bT3/2b=5.2105ZlnΛ \eta = \frac{b}{T^{3/2}} \qquad b = 5.2 \cdot 10^{-5} Z \ln \Lambda

Ohmic heating balancing cross field thermal conduction

Let's consider a region of plasma (radius a a and length L L and estimate the parameters required to achieve a balance between ohmic heating and the cross-field thermal conduction.

The thermal conduction power is

Q2πaL Q 2 \pi a L

The ohmic heating is

ηj2πa2L \eta j^2 \pi a^2 L

κTa/2=ηλ2B2aμ022×B=λB=μ0j \kappa \frac{T}{a/2} = \eta \frac{\lambda^2 B^2 a}{\mu_0 ^2 2} \qquad \curl B = \lambda B = \mu_0 j

Cn2TT1/2B2=bB2T3/222μ02λ2a2κ=Cn2T1/2B2η=bT3/2 \frac{C n^2 T}{T^{1/2} B^2} = \frac{b B^2}{T^{3/2} 2^2 \mu_0 ^2} \lambda ^2 a ^2 \qquad \kappa_\perp = C \frac{n^2}{T^{1/2}B^2} \qquad \eta = \frac{b}{T^{3/2}}

β2(2knT)2(B2/2μ0)2=4k2bCλ2a2 \beta ^2 \equiv \frac{(2 k n T)^2}{(B^2/2 \mu_0)^2} = 4 k^2 \frac{b}{C} \lambda ^2 a^2

where β \beta is the ratio of the plasma pressure p=2nkT p = 2 n k T (the factor of 2 accounts for both species in the plasma) to the magnetic pressure pmag=B2/2μ0 p_{mag} = B^2 / 2 \mu_0 .

For Z=1 Z = 1 and Ai=2 A_i = 2 ,

β=0.15λa \rightarrow \beta = 0.15 \lambda a

λa2.4 \lambda a \approx 2.4 for spheromak, but only 0.5 \approx 0.5 for tokamak.

Axial thermal conduction cools ohmic heating

Consider a voltage applied parallel to the magnetic field

Figure 11.4

Assume that the length is short enough that cross field transport is small compared to axial loss

Q=κdTdXκAT5/2 Q = - \kappa \dv{T}{X} \qquad \kappa \approx A T^{5/2}

Let's just ignore the temperature dependence of Λ \Lambda (since it is slowly varying). Also assume that a current density j j is being driven and the system is in a steady state.

dQdX=ηj2η=bT3/2 \dv{Q}{X} = \eta j^2 \qquad \eta = \frac{b}{T^{3/2}}

b=5.2105ZlnΛ b = 5.2 \cdot 10^{-5} Z \ln \Lambda

Make things dimensionless by normalizing X X by b/Aj/T05/2 \sqrt{b/A} j/T_0 ^{5/2} , q q by Q/AbT0j -Q/\sqrt{Ab}T_0 j and T T by T0 T_0 .

x=XbAjT05/2 x = X \sqrt{\frac{b}{A}} \frac{j}{T_0 ^{5/2}}

q=QT0jAb q = \frac{-Q}{T_0 j \sqrt{Ab}}

T=TT0 T = \frac{T}{T_0}

Q=AT5/2dTdX \rightarrow Q = - A T^{5/2} \dv{T}{X}

dQdX=bT3/2j2 \dv{Q}{X} = \frac{b}{T^{3/2}} j^2

QAT5/2=dTdX - \frac{Q}{A T^{5/2}} = \dv{T}{X}

Replacing the dimensionless quantities,

qT5/2=dTdx \rightarrow \frac{q}{T^{5/2}} = \dv{T}{x}

dQdX=ηj2=bT3/2j2 \dv{Q}{X} = \eta j^2 = \frac{b}{T^{3/2}} j^2

dqdx=1T3/2 \rightarrow - \dv{q}{x} = \frac{1}{T^{3/2}}

Write equation in terms of T0 T_0

AbT0j=Q \sqrt{Ab} T_0 j = - Q

This is Q Q into one electrode

Power per unit area going into the wall is equal to power per unit area in terms of the voltage

AbT0j=Vj2 \sqrt{Ab} T_0 j = \frac{V j}{2}

4ABT0=V \sqrt{4AB} T_0 = V

T0=V4AbV6 T_0 = \frac{V}{\sqrt{4Ab}} \approx \frac{V}{\sqrt{6}}

True for anything without losses across the electrodes.

Viscosity

The shear force is written as

Pyx=μuxy P_{yx} = - \mu \pdv{u_x}{y}

Viscosity is a force per unit area with the force parallel to the surface. It tends to make things want to go the same velocity. It comes about by particles exchanging across the surface

μB=0T5/2Ai1/24ZlnΛ \mu_{B=0} \propto \frac{T^{5/2} A_i ^{1/2}}{4Z\ln \Lambda}

μBni2Z2T1/2B2Ai3/2lnΛ \mu_B \propto \frac{n_i ^2 Z^2}{T^{1/2} B^2} A_i ^{3/2} \ln \Lambda