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Lecture 8
The Solar Wind and Parker Spiral: Dynamic Equilibrium

Overview

Why this lecture matters. The solar wind is one of the cleanest examples of a global MHD equilibrium that is not static. This lecture has four jobs:

1.
show why a sufficiently hot corona cannot remain hydrostatic;
2.
derive Parker’s transonic wind carefully enough that the critical-point logic is unmistakable;
3.
extend the outflow to a rotating, magnetized wind and derive the Parker spiral; and
4.
connect the astrophysical picture back to laboratory experiments that reproduce the same field-line geometry and current-sheet physics.

The heliosphere is not a static atmosphere surrounding the Sun. It is a driven plasma system in which thermal pressure, gravity, magnetic tension, and rotation organize a continuous outflow over astronomical distances. In that sense the solar wind is an ideal lecture for these notes: the mathematics is compact, the physics is global, and the payoff is visible everywhere from space-weather measurements near Earth to laboratory Parker-spiral experiments Parker [1958], Fox et al. [2016], Peterson et al. [2019].

Historical Perspective

Parker’s 1958 insight was radical in exactly the right way: if the corona is hot enough, one should stop forcing a static atmosphere onto it and instead solve for a steady outflow that passes through a sonic critical point Parker [1958]. Once the Sun’s rotation and magnetic field are added, the same outflow naturally winds the field into the Archimedean spiral now called the Parker spiral. The idea was so influential because it explained several solar-system-scale observations at once: a persistent outflow, an interplanetary magnetic field, and a global magnetic geometry shaped by rotation.

8.1 Why a hot corona cannot stay hydrostatic

Before solving for the wind, it is worth seeing why a globally hydrostatic corona fails. Take the momentum equation (1.8) with \[ \uvec = 0, \qquad \J \times \B \approx 0, \qquad \vect {g} = -\frac {GM_\odot }{r^2}\,\vect {e}_r, \] and assume an isothermal equation of state \[ P = c_s^2 \rho , \qquad c_s^2 = \frac {k_B T}{m} = \text {const}. \] Then hydrostatic balance gives

\[\dd {P}{r} = -\rho \frac {GM_\odot }{r^2}. \tag{8.1}\]
Substituting \(P=c_s^2\rho \) into (8.1) yields
\[c_s^2\dd {\rho }{r} = -\rho \frac {GM_\odot }{r^2}, \qquad \frac {1}{\rho }\dd {\rho }{r} = -\frac {GM_\odot }{c_s^2 r^2}. \tag{8.2}\]
Integrating from the coronal base \(R_\odot \) to radius \(r\),
\[\int _{\rho (R_\odot )}^{\rho (r)} \frac {d\rho '}{\rho '} = -\frac {GM_\odot }{c_s^2} \int _{R_\odot }^{r} \frac {dr'}{r'^2},\]
so
\[\ln \!\left [\frac {\rho (r)}{\rho (R_\odot )}\right ] = \frac {GM_\odot }{c_s^2} \left ( \frac {1}{r}-\frac {1}{R_\odot } \right ),\]
and therefore
\[\boxed { \rho (r)=\rho (R_\odot ) \exp \!\left [ \frac {GM_\odot }{c_s^2} \left ( \frac {1}{r}-\frac {1}{R_\odot } \right ) \right ]. } \tag{8.5}\]
As \(r\to \infty \), the exponential tends to a nonzero constant,
\[\rho (\infty )=\rho (R_\odot ) \exp \!\left (-\frac {GM_\odot }{c_s^2R_\odot }\right ) \neq 0. \tag{8.6}\]
So an isothermal hydrostatic corona does not relax toward vacuum at infinity; it approaches a finite density and therefore demands a finite confining pressure at arbitrarily large radius. Parker’s point was that this is not a pathology of the algebra. It is the algebra telling us that a sufficiently hot corona must expand.

Caution

Do not confuse equilibrium with stasis. The solar wind is a steady solution, but not a static one. In a dynamic equilibrium, \[ \pp {}{t}=0, \qquad (\uvec \cdot \grad )\uvec \neq 0, \] so conserved fluxes balance forces along streamlines even while the plasma accelerates.

8.2 Hydrodynamic Parker wind

We now solve the steady, spherically symmetric outflow problem.

Assumptions

The isothermal closure is not the only choice. The conservative energy equation derived earlier can also be reduced to an adiabatic or polytropic closure; see, for example, (3.11). But the isothermal model keeps the critical-point structure completely transparent, so it is the standard first derivation.

Continuity equation Starting from mass conservation (1.7),

\[\divergence (\rho \uvec )=0,\]
spherical symmetry gives
\[\frac {1}{r^2}\dd {}{r}\left (r^2\rho u_r\right )=0.\]
Therefore
\[\boxed { F_m \equiv r^2\rho u_r = \text {const} } \tag{8.9}\]
or, if one prefers to keep the full spherical area explicitly,
\[\dot M_\odot = 4\pi r^2\rho u_r = 4\pi F_m. \tag{8.10}\]
Taking the logarithmic derivative of (8.9),
\[\dd {}{r}\ln (r^2\rho u_r)=0,\]
so
\[\frac {1}{\rho }\dd {\rho }{r} + \frac {1}{u_r}\dd {u_r}{r} + \frac {2}{r} =0.\]
Hence
\[\boxed { \frac {1}{\rho }\dd {\rho }{r} = -\frac {1}{u_r}\dd {u_r}{r} -\frac {2}{r}. } \tag{8.13}\]

Radial momentum equation With no magnetic force yet included, the radial component of (1.8) is

\[\rho u_r\dd {u_r}{r} = -\dd {P}{r} - \rho \frac {GM_\odot }{r^2}. \tag{8.14}\]
For an isothermal gas,
\[P=c_s^2\rho , \qquad \dd {P}{r}=c_s^2\dd {\rho }{r}.\]
Dividing (8.14) by \(\rho \) gives
\[u_r\dd {u_r}{r} = -c_s^2\frac {1}{\rho }\dd {\rho }{r} - \frac {GM_\odot }{r^2}.\]
Now substitute (8.13):
\[\begin{aligned}u_r\dd {u_r}{r} &= -c_s^2 \left ( -\frac {1}{u_r}\dd {u_r}{r}-\frac {2}{r} \right ) - \frac {GM_\odot }{r^2} \\[0.4em] &= \frac {c_s^2}{u_r}\dd {u_r}{r} + \frac {2c_s^2}{r} - \frac {GM_\odot }{r^2}.\end{aligned}\]

Move the derivative terms to the left:

\[\left ( u_r-\frac {c_s^2}{u_r}\right )\dd {u_r}{r} = \frac {2c_s^2}{r} - \frac {GM_\odot }{r^2}.\]
Multiplying by \(u_r\) gives the standard Parker equation,
\[\boxed { \left (u_r^2-c_s^2\right ) \frac {1}{u_r}\dd {u_r}{r} = \frac {2c_s^2}{r} - \frac {GM_\odot }{r^2}. } \tag{8.20}\]
This is the key differential equation of the hydrodynamic wind.

Dimensionless form and integral curve Define the sonic radius

\[r_c = \frac {GM_\odot }{2c_s^2}, \tag{8.21}\]
and dimensionless variables
\[v=\frac {u_r}{c_s}, \qquad x=\frac {r}{r_c}. \tag{8.22}\]
Then (8.20) becomes
\[\boxed { \left (v^2-1\right )\frac {1}{v}\dd {v}{x} = \frac {2}{x}-\frac {2}{x^2}. } \tag{8.23}\]
Now separate variables:
\[\left (v-\frac {1}{v}\right )dv = \left (\frac {2}{x}-\frac {2}{x^2}\right )dx.\]
Integrating both sides,
\[\int \left (v-\frac {1}{v}\right )dv = \int \left (\frac {2}{x}-\frac {2}{x^2}\right )dx,\]
gives
\[\frac {v^2}{2}-\ln v = 2\ln x+\frac {2}{x}+C_1.\]
Multiplying by \(2\) and absorbing constants,
\[\boxed { v^2-\ln v^2 = 4\ln x+\frac {4}{x}+C. } \tag{8.27}\]
This implicit formula contains an entire one-parameter family of steady solutions. The physics lies in deciding which branch is admissible.

Critical point and transonic selection At the radius \(r=r_c\), the right-hand side of (8.20) vanishes. For the derivative to remain finite, the left-hand side must vanish as well, so the smooth solution must satisfy

\[u_r(r_c)=c_s. \tag{8.28}\]
Equivalently, in dimensionless variables the critical point is
\[x=1, \qquad v=1. \tag{8.29}\]
Substituting (8.29) into (8.27) determines the integration constant for the transonic Parker solution:
\[1-\ln 1 = 4\ln 1 + 4 + C \qquad \Longrightarrow \qquad C=-3. \tag{8.30}\]
Thus the physical transonic branch is
\[\boxed { v^2-\ln v^2 = 4\ln x+\frac {4}{x}-3. } \tag{8.31}\]

It is also useful to know the slope at the sonic point. Set

\[x=1+\epsilon , \qquad v=1+\alpha \epsilon , \qquad |\epsilon |\ll 1. \tag{8.32}\]
Then
\[v^2-1 \simeq 2\alpha \epsilon , \qquad \frac {1}{v}\frac {dv}{dx} \simeq \alpha ,\]
so the left-hand side of (8.23) is approximately
\[\left (v^2-1\right )\frac {1}{v}\frac {dv}{dx} \simeq 2\alpha ^2\epsilon .\]
Meanwhile the right-hand side is
\[\begin{aligned}\frac {2}{x}-\frac {2}{x^2} &= \frac {2}{1+\epsilon }-\frac {2}{(1+\epsilon )^2} \nonumber \\ &\simeq 2(1-\epsilon )-2(1-2\epsilon ) \nonumber \\ &\simeq 2\epsilon .\end{aligned}\]

Therefore

\[2\alpha ^2\epsilon = 2\epsilon \qquad \Longrightarrow \qquad \alpha =\pm 1. \tag{8.36}\]
The \(\alpha =+1\) branch is the accelerating solar wind; the \(\alpha =-1\) branch is the accretion-like branch.

Why the other steady branches fail The transonic solution is not just elegant; it is the only steady branch that connects sensible inner and outer boundary conditions.

Breeze branch. For a purely subsonic branch, \(v\ll 1\) at large \(x\), and (8.27) becomes

\[-\ln v^2 \sim 4\ln x, \qquad v\sim x^{-2} \qquad (x\to \infty ). \tag{8.37}\]
Using mass conservation (8.9),
\[\rho = \frac {F_m}{u_r r^2} = \frac {F_m}{c_s v r_c^2 x^2}.\]
Since \(v\sim x^{-2}\), the factor \(v x^2\) tends to a constant, and therefore
\[\rho \to \text {constant} \qquad (r\to \infty ). \tag{8.39}\]
So the breeze solution again requires a finite confining pressure at infinity. It cannot match empty interplanetary space.

Supersonic branch from the base. A purely supersonic solution would require the flow to start above the sound speed at the coronal base, which is inconsistent with the expected low-altitude boundary conditions.

Large-radius transonic asymptotic. For the Parker branch itself, \(v\gg 1\) at large \(x\), so (8.31) gives

\[v^2 \sim 4\ln x, \qquad u_r \sim 2c_s\sqrt {\ln \left (\frac {r}{r_c}\right )}. \tag{8.40}\]
The isothermal solution therefore accelerates only logarithmically at large \(r\), but it does remain supersonic.


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Figure 8.1: Families of steady solutions of the isothermal Parker wind equation. Only the transonic branch passes smoothly through the sonic point and connects realistic boundary conditions at the Sun and at large radius.

Remark on polytropic flow. The isothermal model is the cleanest analytic benchmark. If instead one uses the adiabatic or polytropic pressure law discussed in (3.11), the sound speed varies with radius and the algebra is less tidy, but the core lesson survives: a smooth transonic solution is again selected by the critical-point condition.

8.3 Magnetized rotating wind: the Weber–Davis invariants

Parker’s classic solar-wind solution shows that a hot corona drives a transonic radial outflow and that a frozen-in solar magnetic field is wound into an increasingly spiral geometry by solar rotation [Parker1958]. In the steady, axisymmetric, ideal-MHD refinement of Weber & Davis [Weber and Davis1967], the equatorial wind is organized by first integrals along a streamline/field line: \(\rho u_r r^2=\mathrm {const}\) and \(B_r r^2=\mathrm {const}\), so the mass loading \(\kappa \equiv \rho u_r/B_r\) is constant; the induction equation gives the field-line angular velocity \(\Omega _F \equiv r^{-1}(u_\phi -u_r B_\phi /B_r)\) (equal to the solar rotation rate in the original Weber–Davis model); the azimuthal momentum equation gives the total specific angular momentum \(L \equiv r\!\left (u_\phi -\frac {B_r B_\phi }{4\pi \rho u_r}\right )=r\!\left (u_\phi -\frac {B_\phi }{4\pi \kappa }\right )\); and integrating the radial equation gives a Bernoulli constant \(E \equiv \tfrac 12(u_r^2+u_\phi ^2)+h-\frac {GM_\odot }{r}-\Omega _F r \frac {B_\phi }{4\pi \kappa }\), with \(h=\int dp/\rho \) or \(h=\gamma p/[(\gamma -1)\rho ]\) for a polytrope. Regularity at the Alfvén point then yields the classic lever-arm relation \(L=\Omega _F r_A^2\), which makes explicit how the magnetic field enforces near-corotation close to the Sun while extracting angular momentum from the wind.

We now restore magnetic field and rotation. The resulting model is still highly idealized, but it is enough to generate the Parker spiral and the magnetic braking torque.

Additional assumptions.

Mass flux and open magnetic flux Continuity still gives

\[\rho u_r r^2 = K = \frac {\dot M_\odot }{4\pi }. \tag{8.41}\]
The divergence-free condition (1.12) gives, for a purely radial field,
\[\frac {1}{r^2}\dd {}{r}\left (r^2 B_r\right )=0 \qquad \Longrightarrow \qquad r^2 B_r = \Phi = \text {const}. \tag{8.42}\]
Thus both the mass flux and the open magnetic flux are constants of the flow.

Azimuthal momentum and total angular momentum Take the \(\phi \) component of the steady momentum equation (1.8). In the present geometry,

\[\rho \left ( u_r\dd {u_\phi }{r}+\frac {u_r u_\phi }{r} \right ) = \frac {1}{\muo }\left ( B_r\dd {B_\phi }{r}+\frac {B_r B_\phi }{r} \right ). \tag{8.43}\]
Both sides can be written as total derivatives:
\[\rho u_r\frac {1}{r}\dd {}{r}(r u_\phi ) = \frac {B_r}{\muo r}\dd {}{r}(r B_\phi ). \tag{8.44}\]
Now multiply by \(r^3\) and use (8.41) and (8.42):
\[(\rho u_r r^2)\dd {}{r}(r u_\phi ) = \frac {(B_r r^2)}{\muo }\dd {}{r}(r B_\phi ),\]
so
\[K\dd {}{r}(r u_\phi ) = \frac {\Phi }{\muo }\dd {}{r}(r B_\phi ). \tag{8.46}\]
Integrating once gives
\[K r u_\phi - \frac {\Phi }{\muo } r B_\phi = K L, \tag{8.47}\]
where \(L\) is a constant. Dividing by \(K\) and re-expressing \(\Phi /K=B_r/(\rho u_r)\) yields
\[\boxed { r\left ( u_\phi - \frac {B_r B_\phi }{\muo \rho u_r} \right )=L. } \tag{8.48}\]
This is the specific total angular momentum: the first term is the matter contribution and the second is the magnetic-stress contribution.

Induction equation and corotation invariant The ideal Ohm law is

\[\E +\uvec \times \B =0. \tag{8.49}\]
In the present geometry, the only nontrivial component is the polar one,
\[E_\theta = -(u_\phi B_r-u_r B_\phi ). \tag{8.50}\]
Because the state is steady and axisymmetric, Faraday’s law (1.10) implies \(\grad \times \E =0\), which in this reduced geometry means
\[\dd {}{r}(rE_\theta )=0. \tag{8.51}\]
Therefore
\[r(u_r B_\phi -u_\phi B_r)=C_\Omega , \tag{8.52}\]
where \(C_\Omega \) is another constant. Evaluate it at the coronal base, where the field line is anchored to the rotating Sun and \(B_\phi (R_\odot )\approx 0\):
\[C_\Omega = -R_\odot u_\phi (R_\odot ) B_r(R_\odot ) = -\Omega _\odot R_\odot ^2 B_r(R_\odot ).\]
Since \(R_\odot ^2 B_r(R_\odot )=\Phi \), we obtain
\[C_\Omega =-\Omega _\odot \Phi . \tag{8.54}\]
Substituting (8.42) then gives
\[\boxed { u_\phi -\frac {u_r B_\phi }{B_r}=\Omega _\odot r. } \tag{8.55}\]
Equation (8.55) is the statement that the field line carries the rotation of its footpoint.

Solve for \(u_\phi \) and \(B_\phi \) Define the radial Alfvén Mach number

\[M_A^2 \equiv \frac {\muo \rho u_r^2}{B_r^2}. \tag{8.56}\]
Also write
\[q\equiv \frac {B_\phi }{B_r}. \tag{8.57}\]
Then (8.48) and (8.55) become
\[\begin{aligned}u_\phi - \frac {u_r q}{M_A^2} &= \frac {L}{r}, \\ u_\phi - u_r q &= \Omega _\odot r.\end{aligned} \tag{8.58}\]

Subtract (8.59) from (8.58):

\[u_r q\left (1-\frac {1}{M_A^2}\right )=\frac {L}{r}-\Omega _\odot r. \tag{8.60}\]
Hence
\[q = \frac {1}{u_r} \frac {M_A^2}{M_A^2-1} \left ( \frac {L}{r}-\Omega _\odot r \right ), \tag{8.61}\]
and therefore
\[B_\phi = \frac {B_r}{u_r} \frac {M_A^2}{M_A^2-1} \left ( \frac {L}{r}-\Omega _\odot r \right ). \tag{8.62}\]
Insert (8.61) into (8.59):
\[\begin{aligned}u_\phi &= \Omega _\odot r + \frac {M_A^2}{M_A^2-1} \left ( \frac {L}{r}-\Omega _\odot r \right ) \\ &= \frac {M_A^2 L/r - \Omega _\odot r}{M_A^2-1}.\end{aligned} \tag{8.64}\]


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Figure 8.2: Field lines viewed from top as derived from \(B_r\) and \(B_\phi \).

Parker Spiral Animation

Watch for how steady radial outflow and solar rotation combine to wind the magnetic field into a trailing spiral, with the field at Earth sitting at an intermediate angle rather than remaining purely radial.

Animated Parker spiral geometry from the Sun to Earth

Animated geometry paired with the Parker-spiral derivation and the estimate of the spiral angle near 1 AU.

These expressions appear singular when \(M_A=1\). The singularity is removed only if the numerators vanish at the same radius. Define the Alfvén point by
\[u_r^2(r_A)=\frac {B_r^2(r_A)}{\muo \rho (r_A)} \qquad \Longleftrightarrow \qquad M_A(r_A)=1. \tag{8.65}\]
Regularity at \(r=r_A\) then requires
\[\frac {L}{r_A}-\Omega _\odot r_A = 0 \qquad \Longrightarrow \qquad L=\Omega _\odot r_A^2. \tag{8.66}\]
Substitute (8.66) into (8.62) and (8.64):
\[\boxed { B_\phi = -\frac {B_r\Omega _\odot r}{u_r} \left [ \frac {1-r_A^2/r^2}{M_A^2-1} \right ]M_A^2, } \tag{8.67}\]
\[\boxed { u_\phi = \Omega _\odot r \left [ \frac {M_A^2 r_A^2/r^2-1}{M_A^2-1} \right ]. } \tag{8.68}\]

These formulas make the physics transparent. Inside the Alfvén radius, \(M_A\ll 1\) and the magnetic field enforces near-corotation, \(u_\phi \approx \Omega _\odot r\). Outside the Alfvén radius, \(M_A\gg 1\) and the plasma inertia dominates, giving

\[u_\phi \approx \frac {\Omega _\odot r_A^2}{r}, \qquad B_\phi \approx -\frac {\Omega _\odot r}{u_r}B_r. \tag{8.69}\]

Maxwell stress and solar spindown The angular-momentum flux per unit solid angle is

\[\mathcal {F}_J = r^3\left (\rho u_r u_\phi - \frac {B_r B_\phi }{\muo }\right ). \tag{8.70}\]
Use (8.48) to rewrite this as
\[\begin{aligned}\mathcal {F}_J &= \rho u_r r^2 \cdot r\left (u_\phi - \frac {B_r B_\phi }{\muo \rho u_r}\right ) \\ &= K L.\end{aligned} \tag{8.72}\]

Multiplying by \(4\pi \) gives the total torque,

\[\dot J = 4\pi \mathcal {F}_J = 4\pi K L = \dot M_\odot L. \tag{8.73}\]
Using (8.66),
\[\boxed { \dot J = \dot M_\odot \,\Omega _\odot \,r_A^2. } \tag{8.74}\]
This is the standard magnetic-braking formula. The Alfvén radius acts as the effective lever arm: matter leaves with modest azimuthal speed, but the magnetic field transmits the corotation torque out to \(r_A\) before the gas fully decouples.


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Figure 8.3: Geometry of a laboratory Parker spiral. The same ideal-MHD ingredients used in the heliosphere—a rotating magnetized plasma and an outward wind—generate a spiral magnetic structure in the laboratory as well Peterson et al. [2019].

8.4 Parker spiral geometry

A magnetic field line is everywhere tangent to \(\B \), so in the equatorial plane

\[\frac {d\phi }{dr} = \frac {B_\phi }{rB_r}. \tag{8.75}\]
Far from the Sun, use (8.69):
\[\frac {d\phi }{dr} \approx -\frac {\Omega _\odot }{u_r}. \tag{8.76}\]
If the wind speed has already saturated to an approximately constant value, integration is immediate:
\[\phi (r)-\phi (r_0) = -\frac {\Omega _\odot }{u_r}(r-r_0). \tag{8.77}\]
Equivalently, absorbing \(r_0\) into the integration constant,
\[\boxed { \phi (r)=\phi _0-\frac {\Omega _\odot }{u_r}r. } \tag{8.78}\]
The field therefore forms an Archimedean spiral.

The angle \(\psi \) between the magnetic field and the radial direction obeys

\[\tan \psi = \frac {|B_\phi |}{B_r}. \tag{8.79}\]
Using the far-field result for \(B_\phi \),
\[\boxed { \tan \psi \approx \frac {\Omega _\odot r}{u_r}. } \tag{8.80}\]
At Earth, with \(u_r\approx 400~\mathrm {km/s}\), \(\Omega _\odot \approx 2.7\times 10^{-6}~\mathrm {s}^{-1}\), and \(r=1~\mathrm {AU}\), one finds \(\tan \psi \approx 1\), so \(\psi \approx 45^\circ \). The interplanetary magnetic field at Earth is therefore neither purely radial nor purely azimuthal; it typically sits at an intermediate spiral angle.

8.5 Experimental and observational perspective

The solar-wind lecture is a good place to remind ourselves that MHD is not separated into astrophysical and laboratory silos. The Parker problem has now been explored in both settings.

On the observational side, the solar wind is the reason space plasma physics exists as a discipline: a magnetized, supersonic plasma stream continuously bathes the planets, drives shocks and current sheets, and communicates solar variability throughout the heliosphere. The Parker Solar Probe mission was designed precisely to move the observational boundary condition inward, toward the region where the wind is accelerated and the spiral field is established Fox et al. [2016].

On the laboratory side, rotating magnetized plasma experiments have reproduced the same qualitative ingredients: a central magnetized source, an outwardly accelerated plasma, and a spiral magnetic geometry produced by frozen-in advection Peterson et al. [2019]. Those experiments also produce current-sheet dynamics and plasmoid ejection in Parker-like geometries Peterson et al. [2021]. This is exactly the kind of cross-scale connection that makes MHD so powerful.


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Figure 8.4: Experimental configuration for a laboratory implementation of the Parker spiral on the Big Red Ball platform. An imposed electric field drives rotation; centrifugal forces launch an outflow; the magnetic field is wound into a spiral; and current sheets can eject plasmoids in close analogy with heliospheric structures Peterson et al. [20192021].

8.6 Outlook: when isotropic pressure is not enough

Everything above assumed a scalar pressure. That is the right place to start, but the real solar wind is only weakly collisional over much of the heliosphere. In that regime the pressure need not remain isotropic, and the later CGL/kinetic lectures become important.

A very simple scaling already shows why. In the collisionless double-adiabatic limit,

\[\frac {p_\perp }{\rho B}=\text {const}, \qquad \frac {p_\parallel B^2}{\rho ^3}=\text {const}. \tag{8.81}\]
For a nearly radial far-zone wind,
\[B_r\propto r^{-2}, \qquad \rho u_r r^2=\text {const}. \tag{8.82}\]
If \(u_r\) is approximately constant once the wind is super-Alfvénic, then \(\rho \propto r^{-2}\) as well. Equation (8.81) then implies
\[p_\perp \propto \rho B \propto r^{-4}, \qquad p_\parallel \propto \frac {\rho ^3}{B^2} \propto r^{-2}. \tag{8.83}\]
Therefore
\[\frac {p_\parallel }{p_\perp }\propto r^2. \tag{8.84}\]
So even if the pressure starts nearly isotropic near the Sun, radial expansion naturally drives anisotropy. That is one reason the solar wind is such a fertile environment for mirror, firehose, and heat-flux physics Hellinger et al. [2006], Bale et al. [2009].

Takeaways
  • A hot corona cannot remain globally hydrostatic. The static isothermal solution leaves a finite density at infinity, so expansion is unavoidable.
  • The steady wind is selected by a critical-point condition. The smooth Parker branch passes through \(u_r=c_s\) at \(r_c=GM_\odot /(2c_s^2)\) and is the only physically acceptable global solution.
  • In ideal MHD, frozen-in flux and solar rotation produce two key invariants: total specific angular momentum (8.48) and field-line corotation (8.55).
  • The Alfvén radius is the magnetic lever arm. It sets both the Parker-spiral geometry and the stellar torque \(\dot J=\dot M_\odot \Omega _\odot r_A^2\).
  • The textbook Parker solution uses isotropic pressure, but heliospheric expansion naturally drives pressure anisotropy, so the solar wind also serves as a gateway to weakly collisional plasma physics.

Bibliography

    E N Parker. Dynamics of the interplanetary gas and magnetic fields. The Astrophysical Journal, 128:664, 1958. doi:10.1086/146579.

    N. J. Fox, M. C. Velli, S. D. Bale, R. Decker, A. Driesman, R. A. Howard, J. C. Kasper, J. Kinnison, M. Kusterer, P. C. Liewer, D. J. McComas, A. Szabo, et al. The solar probe plus mission: Humanity’s first visit to our star. Space Science Reviews, 204(1–4):7–48, 2016. doi:10.1007/s11214-015-0211-6.

    Ethan E. Peterson, Douglass A. Endrizzi, Matthew Beidler, Kyle J. Bunkers, Michael Clark, Jan Egedal, Ken Flanagan, Karsten J. McCollam, Jason Milhone, Joseph Olson, Carl R. Sovinec, Roger Waleffe, John Wallace, and Cary B. Forest. A laboratory model for the parker spiral and magnetized stellar winds. Nature Physics, 15(10):1095–1100, 2019. doi:10.1038/s41567-019-0592-7.

    Edmund J. Weber and Leverett Davis, Jr. The angular momentum of the solar wind. The Astrophysical Journal, 148:217–227, 1967. doi:10.1086/149138.

    Ethan E. Peterson, Douglass A. Endrizzi, Michael Clark, Jan Egedal, Kenneth Flanagan, Nuno F. Loureiro, Jason Milhone, Joseph Olson, Carl R. Sovinec, John Wallace, and Cary B. Forest. Laminar and turbulent plasmoid ejection in a laboratory parker spiral current sheet. Journal of Plasma Physics, 87(4):905870410, 2021. doi:10.1017/s0022377821000775.

    P. Hellinger, P. Trávníček, J. C. Kasper, and A. J. Lazarus. Solar wind proton temperature anisotropy: Linear theory and WIND/SWE observations. Geophysical Research Letters, 33: L09101, 2006. doi:10.1029/2006GL025925.

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Problems

Problem 8.1. Parker Wind, Parker Spiral, and Magnetic Braking

Part A: global Parker wind Start from the steady isothermal wind equation

\[\left (u^2-c_s^2\right )\frac {1}{u}\frac {du}{dr} = \frac {2c_s^2}{r}-\frac {GM_\odot }{r^2}.\]
Define
\[v=\frac {u}{c_s}, \qquad x=\frac {r}{r_c}, \qquad r_c=\frac {GM_\odot }{2c_s^2}.\]

A1. Show carefully that the equation becomes

\[\left (v^2-1\right )\frac {1}{v}\frac {dv}{dx} = \frac {2}{x}-\frac {2}{x^2}.\]
Then separate variables and derive the first integral
\[v^2-\ln v^2=4\ln x+\frac {4}{x}+C.\]
Determine the constant \(C\) for the transonic Parker solution.

A2. Expand about the sonic point by writing \[ x=1+\epsilon , \qquad v=1+\alpha \epsilon , \qquad |\epsilon |\ll 1. \] Show that \(\alpha =\pm 1\) and explain why the \(+\) branch corresponds to the solar wind.

A3. Using a numerical integrator (Python, MATLAB, Julia, etc.), integrate the wind equation from a point slightly displaced from the sonic point. Plot several nearby branches and identify:

A4. Show analytically that for the breeze branch \(v\sim x^{-2}\) at large radius. Then use mass conservation to prove that \(\rho \to \text {constant}\) as \(r\to \infty \), and explain why this requires an external confining pressure.

Part B: angular momentum invariants Assume a steady, axisymmetric, ideal-MHD wind in the equatorial plane, with \[ \rho u_r r^2=K, \qquad B_r r^2=\Phi . \]

B1. Starting from

\[\rho \left (u_r\frac {du_\phi }{dr}+\frac {u_r u_\phi }{r}\right ) = \frac {1}{\muo }\left (B_r\frac {dB_\phi }{dr}+\frac {B_rB_\phi }{r}\right ),\]
show step by step that
\[r\left (u_\phi -\frac {B_rB_\phi }{\muo \rho u_r}\right )=L,\]
where \(L\) is constant.

B2. Starting from the ideal Ohm law,

\[\E +\uvec \times \B =0,\]
and using steady axisymmetry, show that
\[u_\phi -\frac {u_rB_\phi }{B_r}=\Omega _\odot r.\]
Explain the physical meaning of this relation.

Part C: Alfvén point and stellar torque Define

\[M_A^2=\frac {\muo \rho u_r^2}{B_r^2}.\]

C1. Solve the two equations from Part B for \(u_\phi \) and \(B_\phi \) in terms of \(M_A\), \(L\), and \(\Omega _\odot \).

C2. Show that regularity at the Alfvén point \(M_A=1\) requires

\[L=\Omega _\odot r_A^2.\]

C3. Show that the total angular momentum loss rate can be written as

\[\dot J = \dot M_\odot L = \dot M_\odot \Omega _\odot r_A^2.\]
Why does \(r_A\) act like a magnetic lever arm?

C4. Using \[ \dot M_\odot \sim 2\times 10^{-14}M_\odot /\mathrm {yr}, \qquad r_A\sim 10R_\odot , \qquad J_\odot \sim 2\times 10^{41}\,\mathrm {kg\,m^2/s}, \] estimate the solar spindown timescale \[ \tau \sim \frac {J_\odot }{\dot J}. \] Comment on the astrophysical significance of your answer.

Part D: spiral angle and weakly collisional expansion

D1. For the far-zone Parker spiral, show that

\[\tan \psi = \frac {|B_\phi |}{B_r}\approx \frac {\Omega _\odot r}{u_r}.\]
Evaluate \(\psi \) at \(1~\mathrm {AU}\) for \[ u_r=400~\mathrm {km/s}, \qquad \Omega _\odot =2.7\times 10^{-6}~\mathrm {s}^{-1}. \] Is the field at Earth closer to radial or azimuthal?

D2. Assume a collisionless far-zone wind with \(u_r\approx \text {const}\), so that \(\rho \propto r^{-2}\) and \(B_r\propto r^{-2}\). Using

\[\frac {p_\perp }{\rho B}=\text {const}, \qquad \frac {p_\parallel B^2}{\rho ^3}=\text {const},\]
show that \(p_\perp \propto r^{-4}\) and \(p_\parallel \propto r^{-2}\). What does this imply for the ratio \(p_\parallel /p_\perp \) as the wind expands?