Radiation

AST1440: Electron Scattering, Eddington Luminosity, and Strong Magnetic Fields

AST1440:电子散射、爱丁顿光度与强磁场

AI-translated edition. Equations and notation are preserved. Refer to the Chinese original for authoritative wording.

Derivations of electron scattering and the Thomson cross section, radiation force and Eddington luminosity, and corrections from strong magnetic fields, beaming, and accretion columns.

28 min readAST1440Electron scatteringEddington luminosity
On this page

Lecture: Monday, September 14, 2026.
Organization: Following the lecture topics, conceptual questions, derivations, intuitive explanations, and common calculation pitfalls are integrated into the relevant sections.
Course website: AST1440 — Radiation. The website changes over time; these notes use the previously checked 2026 schedule. The 2025 thermal-radiation schedule, initially read in error, is not included in this lecture's scope.

1. Main thread and reading scope

The central questions are: Why does light push matter? Why does this limit astronomical luminosities? How do strong magnetic fields change that limit?

The physical sequence is:

Light accelerates electrons⟶Electrons scatter light and exchange momentum⟶Radiation force competes with gravity⟶LEdd⟶Corrections from strong magnetic fields and nonspherical geometry.\text{Light accelerates electrons} \longrightarrow\text{Electrons scatter light and exchange momentum} \longrightarrow\text{Radiation force competes with gravity} \longrightarrow L_{\rm Edd} \longrightarrow\text{Corrections from strong magnetic fields and nonspherical geometry}.

The assigned reading is Rybicki & Lightman (RL), §§1.1–1.4; class discussion emphasizes Problem 1.4 and its ULX extension. Supplementary electron-scattering references are Padmanabhan (Pad), §§1.4.4 and 6.4, or RL §§3.4 and 3.6. Material on thermal radiation from September 17, 2026 is not mixed into these notes.

The detailed derivations fill gaps in understanding; their inclusion does not mean that the course website records every derivation step.

2. Notation and unit systems: distinguish easily confused quantities

SymbolMeaning
e>0e>0Magnitude of the electron charge; the electron's charge is −e-e
me,mpm_e,m_pElectron and proton masses
E0E_0Peak electric-field amplitude of the wave, not its rms value
B0\mathbf B_0Applied or background magnetic field, distinguished from the wave's own field
PscP_{\rm sc}Total power scattered by one particle into all directions
FFLocal energy flux, in erg cm−2 s−1{\rm erg\,cm^{-2}\,s^{-1}}
fobsf_{\rm obs}Energy flux measured by the observer
LLTotal luminosity, in erg s−1{\rm erg\,s^{-1}}
σ\sigmaSingle-particle scattering cross section, in cm2{\rm cm^2}
κ\kappaOpacity per unit mass, in cm2 g−1{\rm cm^2\,g^{-1}}
ρ\rhoMass density of matter
gradg_{\rm rad}Radiative acceleration: radiation force per unit mass
ω,ωB\omega,\omega_BWave angular frequency and electron cyclotron angular frequency

Unless explicitly labeled SI, all equations below use Gaussian-cgs units.

2.1 Why is the magnetic Lorentz-force term divided by cc?

The two unit systems use different expressions:

Gaussian-cgs:F=q(E+v×Bc),SI:F=q(E+v×B).\begin{aligned} \text{Gaussian-cgs:}\quad \mathbf F&=q\left(\mathbf E+\frac{\mathbf v\times\mathbf B}{c}\right),\\ \text{SI:}\quad \mathbf F&=q(\mathbf E+\mathbf v\times\mathbf B). \end{aligned}

This reflects different unit definitions, not different physical laws. In Gaussian-cgs, EE and BB have the same dimensions, so the dimensionless factor v/cv/c is needed to add the two terms. In SI, vBvB already has the same dimensions as EE:

[vB]=msV sm2=V/m=[E].[vB]=\frac{\rm m}{\rm s}\frac{{\rm V\,s}}{{\rm m^2}}={\rm V/m}=[E].

A plane wave in vacuum satisfies:

E=B(cgs),E=cB(SI).E=B\quad\text{(cgs)},\qquad E=cB\quad\text{(SI)}.

Thus, comparing the wave's own electric and magnetic forces gives the same order-of-magnitude ratio in both systems:

FBFE∼vc.\frac{F_B}{F_E}\sim\frac vc.

For a nonrelativistic electron, the wave's own magnetic force is a higher-order effect that may be neglected. This does not justify neglecting an independently present strong background field B0\mathbf B_0.

2.2 Common formulas in the two unit systems

Physical quantityGaussian-cgsSI
Poynting vectorS=cE×B/(4π)\mathbf S=c\mathbf E\times\mathbf B/(4\pi)S=E×B/μ0\mathbf S=\mathbf E\times\mathbf B/\mu_0
Magnetic energy densityuB=B2/(8π)u_B=B^2/(8\pi)uB=B2/(2μ0)u_B=B^2/(2\mu_0)
Electron cyclotron angular frequencyωB=eB/(mec)\omega_B=eB/(m_ec)ωB=eB/me\omega_B=eB/m_e
Larmor powerP=2q2a2/(3c3)P=2q^2a^2/(3c^3)P=q2a2/(6πε0c3)P=q^2a^2/(6\pi\varepsilon_0c^3)
Classical electron radiusre=e2/(mec2)r_e=e^2/(m_ec^2)re=e2/(4πε0mec2)r_e=e^2/(4\pi\varepsilon_0m_ec^2)

Using values consistently within either unit system gives the same physical result. Do not insert BB measured in gauss directly into an SI formula.

3. How is the average incident energy flux calculated?

3.1 Starting from the Poynting vector

Consider a vacuum plane wave propagating along +z+z:

E=E0cos⁡(kz−ωt) x^,B=E0cos⁡(kz−ωt) y^.\mathbf E=E_0\cos(kz-\omega t)\,\hat{\mathbf x},\qquad \mathbf B=E_0\cos(kz-\omega t)\,\hat{\mathbf y}.

The electric and magnetic fields are perpendicular and in phase, with equal magnitudes in cgs. The Poynting vector represents electromagnetic energy passing per unit area per unit time:

S=c4πE×B=cE024πcos⁡2(kz−ωt) z^.\mathbf S=\frac{c}{4\pi}\mathbf E\times\mathbf B =\frac{cE_0^2}{4\pi}\cos^2(kz-\omega t)\,\hat{\mathbf z}.

For an area perpendicular to propagation, the instantaneous flux is

F(t)=cE024πcos⁡2(kz−ωt).F(t)=\frac{cE_0^2}{4\pi}\cos^2(kz-\omega t).

Since

cos⁡2x=1+cos⁡2x2,⟨cos⁡2ωt⟩=12,\cos^2x=\frac{1+\cos2x}{2},\qquad \langle\cos^2\omega t\rangle=\frac12,

the cycle-averaged flux is

⟨F⟩=cE028π.\boxed{\langle F\rangle=\frac{cE_0^2}{8\pi}}.

The factor 1/21/2 comes from time averaging. If Erms=E0/2E_{\rm rms}=E_0/\sqrt2 is used instead, write

⟨F⟩=cErms24π.\langle F\rangle=\frac{cE_{\rm rms}^2}{4\pi}.

The corresponding SI result is ⟨F⟩=ε0cE02/2\langle F\rangle=\varepsilon_0cE_0^2/2.

3.2 Energy density times propagation speed

The electromagnetic energy density is

u=E2+B28π=E24π,⟨u⟩=E028π.u=\frac{E^2+B^2}{8\pi}=\frac{E^2}{4\pi}, \qquad \langle u\rangle=\frac{E_0^2}{8\pi}.

During dtdt, the wave in a length c dtc\,dt in front of area AA crosses that area, corresponding to volume Ac dtAc\,dt. Therefore

⟨F⟩=⟨u⟩Ac dtA dt=c⟨u⟩=cE028π.\langle F\rangle =\frac{\langle u\rangle Ac\,dt}{A\,dt} =c\langle u\rangle =\frac{cE_0^2}{8\pi}.

4. Why do accelerated charges radiate? Deriving the Larmor formula

4.1 Starting with the far-zone radiation field

The far-zone radiation electric field of a nonrelativistically accelerated charge is

Erad=qc2r[n^×(n^×a)]ret.\mathbf E_{\rm rad} =\frac{q}{c^2r} \left[\hat{\mathbf n}\times(\hat{\mathbf n}\times\mathbf a)\right]_{\rm ret}.

This follows from Maxwell's equations or retarded potentials and serves as the electrodynamic starting point. Here n^\hat{\mathbf n} points toward the observer; the subscript 'ret' means that the acceleration is evaluated at the retarded time.

If the angle between the observation direction and acceleration is θ\theta, then

Erad=∣q∣asin⁡θc2r.E_{\rm rad}=\frac{|q|a\sin\theta}{c^2r}.

The radiation field falls as 1/r1/r, unlike the Coulomb field, which falls as 1/r21/r^2. It can thus carry finite total outward power to large distances.

4.2 Power in each direction from the radiation field

The far-zone radiation field satisfies Brad=n^×Erad\mathbf B_{\rm rad}=\hat{\mathbf n}\times\mathbf E_{\rm rad}, so

S=c4πErad2=q2a2sin⁡2θ4πc3r2.S=\frac{c}{4\pi}E_{\rm rad}^2 =\frac{q^2a^2\sin^2\theta}{4\pi c^3r^2}.

A spherical surface element has area dA=r2dΩdA=r^2d\Omega, and the power through it is

dP=S dA,dPdΩ=q2a24πc3sin⁡2θ.dP=S\,dA, \qquad \frac{dP}{d\Omega}=\frac{q^2a^2}{4\pi c^3}\sin^2\theta.

There is therefore no radiation along the acceleration direction; radiation is strongest perpendicular to it.

4.3 Integrating over the whole sphere

P=q2a24πc3∫sin⁡2θ dΩ,∫sin⁡2θ dΩ=∫02πdϕ∫0πsin⁡3θ dθ=2π×43=8π3.\begin{aligned} P&=\frac{q^2a^2}{4\pi c^3}\int\sin^2\theta\,d\Omega,\\ \int\sin^2\theta\,d\Omega &=\int_0^{2\pi}d\phi\int_0^\pi\sin^3\theta\,d\theta =2\pi\times\frac43=\frac{8\pi}{3}. \end{aligned}

This yields

P=2q2a23c3.\boxed{P=\frac{2q^2a^2}{3c^3}}.

The coefficient 2/32/3 comes from integrating the angular radiation pattern over the sphere. The formula gives instantaneous total power at the corresponding emission time, not an automatically cycle-averaged result.

Only if a(t)=a0cos⁡ωta(t)=a_0\cos\omega t do we further obtain

⟨P⟩=2q23c3⟨a2⟩=q2a023c3.\boxed{\langle P\rangle=\frac{2q^2}{3c^3}\langle a^2\rangle =\frac{q^2a_0^2}{3c^3}}.

This form applies to nonrelativistic motion and cannot be used directly near the speed of light.

5. Scattering cross sections, the Thomson derivation, and the classical electron radius

5.1 What is a scattering cross section? The rain-collection analogy

Imagine incident light as rain and the target's interaction with light as collecting water:

water collected per second=rainfall intensity×bucket opening area.\text{water collected per second} =\text{rainfall intensity}\times\text{bucket opening area}.

For scattering, the analogous relation is

total scattered power=incident energy flux×scattering cross section.\text{total scattered power} =\text{incident energy flux}\times\text{scattering cross section}.

Thus define

σ=⟨Psc⟩⟨Finc⟩.\boxed{\sigma=\frac{\langle P_{\rm sc}\rangle}{\langle F_{\rm inc}\rangle}}.

For example, with incident flux 100 W m−2100\ {\rm W\,m^{-2}}, a target scattering total power 2 W2\ {\rm W} has cross section 0.02 m20.02\ {\rm m^2}. Its scattered power equals the incident power passing through an area of that size.

This is an effective area defined by the interaction's effect, not necessarily the target's geometric area. It is not a sharply bounded circle inside which all light scatters and outside which nothing happens.

For an electron, the light's electric field drives oscillations and the electron reradiates. At fixed incident light, stronger reradiation means a larger cross section. If a magnetic field weakens certain responses, the cross section decreases, but the electron itself has not shrunk.

Dimensional check:

[σ]=erg s−1erg cm−2 s−1=cm2.[\sigma]=\frac{{\rm erg\,s^{-1}}}{{\rm erg\,cm^{-2}\,s^{-1}}}={\rm cm^2}.

5.2 Conditions for the Thomson limit

  • Free electrons: no restoring force from binding.
  • Nonrelativistic response: electron speeds are much smaller than cc; the wave must not be strong enough to drive relativistic motion.
  • Low photon energy: in the electron's initial rest frame, hν≪mec2≃511 keVh\nu\ll m_ec^2\simeq511\ {\rm keV}, so recoil energy changes are negligible.
  • Ordinary, unmagnetized response: no strong background magnetic-field effect needs to be retained.

Under these conditions, the electron can be treated as a classical charge driven by the incident wave.

5.3 Step 1: The electric field drives the electron

Write the incident electric field at the electron as

E(t)=E0cos⁡ωt x^.\mathbf E(t)=E_0\cos\omega t\,\hat{\mathbf x}.

Neglect the relatively small magnetic force of the wave:

mex¨=−eE0cos⁡ωt,a(t)=−eE0mecos⁡ωt.m_e\ddot x=-eE_0\cos\omega t, \qquad a(t)=-\frac{eE_0}{m_e}\cos\omega t.

Defining acceleration amplitude a0=eE0/mea_0=eE_0/m_e gives

⟨a2⟩=a022=e2E022me2.\langle a^2\rangle=\frac{a_0^2}{2} =\frac{e^2E_0^2}{2m_e^2}.

5.4 Step 2: The electron radiates

Substitute into the Larmor formula:

⟨Psc⟩=2e23c3⟨a2⟩=2e23c3e2E022me2=e4E023me2c3.\begin{aligned} \langle P_{\rm sc}\rangle &=\frac{2e^2}{3c^3}\langle a^2\rangle\\ &=\frac{2e^2}{3c^3}\frac{e^2E_0^2}{2m_e^2} =\boxed{\frac{e^4E_0^2}{3m_e^2c^3}}. \end{aligned}

5.5 Step 3: Divide by the mean incident flux

σT=⟨Psc⟩⟨Finc⟩=e4E023me2c38πcE02=8πe43me2c4≃6.65×10−25 cm2.\begin{aligned} \sigma_{\rm T} &=\frac{\langle P_{\rm sc}\rangle}{\langle F_{\rm inc}\rangle}\\ &=\frac{e^4E_0^2}{3m_e^2c^3}\frac{8\pi}{cE_0^2}\\ &=\boxed{\frac{8\pi e^4}{3m_e^2c^4}} \simeq6.65\times10^{-25}\ {\rm cm^2}. \end{aligned}

The field strength E0E_0 cancels because both scattered power and incident flux are proportional to E02E_0^2. Frequency does not appear because the free-electron acceleration amplitude eE0/meeE_0/m_e is frequency-independent in this approximation.

5.6 Common mistake: Why might one obtain 16π16\pi?

The most common cause is using peak radiated power in the numerator but average incident flux in the denominator.

This inconsistent combination gives

2e4E02/(3me2c3)⏞peak powercE02/(8π)⏟mean flux=16πe43me2c4.\frac{\overbrace{2e^4E_0^2/(3m_e^2c^3)}^{\text{peak power}}} {\underbrace{cE_0^2/(8\pi)}_{\text{mean flux}}} =\frac{16\pi e^4}{3m_e^2c^4}.

Use consistent quantities in numerator and denominator:

Quantities usedScattered powerIncident flux
Peak values2e4E02/(3me2c3)2e^4E_0^2/(3m_e^2c^3)cE02/(4π)cE_0^2/(4\pi)
Cycle averagese4E02/(3me2c3)e^4E_0^2/(3m_e^2c^3)cE02/(8π)cE_0^2/(8\pi)

In this sinusoidally driven model, taking the ratio consistently within either row yields 8πe4/(3me2c4)8\pi e^4/(3m_e^2c^4). The factor 22 in the Larmor formula is canceled by ⟨cos⁡2⟩=1/2\langle\cos^2\rangle=1/2 in the average power.

5.7 Why define the classical electron radius?

Define

re≡e2mec2≃2.818×10−13 cm=2.818 fm.\boxed{r_e\equiv\frac{e^2}{m_ec^2}} \simeq2.818\times10^{-13}\ {\rm cm}=2.818\ {\rm fm}.

This comes from a natural comparison of energy scales. Two charges of magnitude ee separated by rr have electrostatic potential-energy magnitude e2/re^2/r. Set this scale equal to the electron rest energy:

e2re=mec2,\frac{e^2}{r_e}=m_ec^2,

This gives the definition above. It does not imply that an electron contains two charges.

Nor should rer_e be interpreted directly as the electron's physical radius. In classical charged-sphere models, electrostatic self-energy depends on the charge distribution:

ModelElectrostatic self-energyRadius obtained by setting self-energy equal to mec2m_ec^2
Uniformly charged spherical shelle2/(2R)e^2/(2R)R=re/2R=r_e/2
Uniformly charged solid sphere3e2/(5R)3e^2/(5R)R=3re/5R=3r_e/5

Thus, rer_e is a well-defined conventional classical electromagnetic length scale, not a unique physical size inferred from these models. The Thomson cross section can be written as

σT=8π3re2.\boxed{\sigma_{\rm T}=\frac{8\pi}{3}r_e^2}.

It measures the driven electron's ability to reradiate, not the geometric area of a solid little sphere struck by light.

6. Deriving radiative acceleration from photon momentum transfer

6.1 From a single-particle cross section to opacity per unit mass

For scatterer number density nn and single-particle cross section σ\sigma, the interaction coefficient per unit length is nσn\sigma. Dividing by mass density gives

κ=nσρ,dτ=nσ ds=κρ ds.\boxed{\kappa=\frac{n\sigma}{\rho}}, \qquad d\tau=n\sigma\,ds=\kappa\rho\,ds.

This first considers one interaction. Multiple species, absorption, and scattering processes require the corresponding sum; radiation-force calculations must use coefficients describing momentum transfer.

6.2 Intercepted energy in a small piece of matter

A thin layer has illuminated area AA, thickness dsds, and density ρ\rho. Its mass is

dm=ρA ds.dm=\rho A\,ds.

Choose dsds small enough that dτ=κρ ds≪1d\tau=\kappa\rho\,ds\ll1. The fraction of light interacting is approximately dτd\tau.

During time dtdt, the incident energy is FA dtFA\,dt; the energy participating in interactions is

dEint=FA dt dτ=FA dt κρ ds.dE_{\rm int}=FA\,dt\,d\tau =FA\,dt\,\kappa\rho\,ds.

6.3 Convert energy to momentum, then divide force by mass

First consider absorption. Since photons satisfy p=E/cp=E/c, matter gains

dp=dEintc=FA dt κρ dsc.dp=\frac{dE_{\rm int}}{c} =\frac{FA\,dt\,\kappa\rho\,ds}{c}.

Force is momentum gained per unit time:

dFrad=dpdt=FAκρ dsc.d\mathcal F_{\rm rad}=\frac{dp}{dt} =\frac{FA\kappa\rho\,ds}{c}.

Dividing by the mass of the material:

grad=dFraddm=FAκρ dscρA ds=κFc.\begin{aligned} g_{\rm rad} &=\frac{d\mathcal F_{\rm rad}}{dm}\\ &=\frac{FA\kappa\rho\,ds}{c\rho A\,ds} =\boxed{\frac{\kappa F}{c}}. \end{aligned}

Area, thickness, and density cancel because intercepting capacity increases in proportion to material mass. Distinguish:

κFc⏟force per unit mass, or accelerationfromρκFc⏟force per unit volume.\underbrace{\frac{\kappa F}{c}}_{\text{force per unit mass, or acceleration}} \qquad\text{from}\qquad \underbrace{\frac{\rho\kappa F}{c}}_{\text{force per unit volume}}.

Dimensional check:

[κFc]=(cm2 g−1)(erg cm−2 s−1)cm s−1=cm s−2.\left[\frac{\kappa F}{c}\right] =\frac{({\rm cm^2\,g^{-1}})({\rm erg\,cm^{-2}\,s^{-1}})}{{\rm cm\,s^{-1}}} ={\rm cm\,s^{-2}}.

6.4 How can scattering exert force without absorbing the light?

Scattering changes photon propagation direction and therefore momentum. Even with approximately unchanged photon energy, momentum can still be transferred to an electron.

For example, a photon scattered through angle θ\theta transfers momentum along the incident direction of

Δp∥=Eγc(1−cos⁡θ).\Delta p_\parallel=\frac{E_\gamma}{c}(1-\cos\theta).

Strictly, radiation force therefore requires the momentum-transfer cross section. Ordinary Thomson scattering has a fore–aft symmetric angular pattern, with angle-averaged cos⁡θ\cos\theta equal to zero. The momentum-transfer cross section equals the total Thomson cross section, so grad=κesF/cg_{\rm rad}=\kappa_{\rm es}F/c still holds.

Strongly forward-peaked scattering or complicated magnetic anisotropy prevents blindly using an arbitrary total scattering cross section for radiation force.

For a frequency distribution describable with scalar opacity, write

grad=1c∫κνFν dν=κFFc,κF≡∫κνFν dν∫Fν dν.g_{\rm rad}=\frac1c\int\kappa_\nu F_\nu\,d\nu =\frac{\kappa_FF}{c}, \qquad \kappa_F\equiv\frac{\int\kappa_\nu F_\nu\,d\nu}{\int F_\nu\,d\nu}.

Here κF\kappa_F is the flux-mean opacity.

An optically thin local layer does not require the entire object to be optically thin. An optically thick medium can be divided into thin layers, with the radiation force calculated from the local net flux.

7. Eddington luminosity: derivation, assumptions, and meaning

7.1 From local flux to total luminosity

Assume spherically symmetric outward radiation. At radius rr, the luminosity is distributed over spherical area 4πr24\pi r^2:

F(r)=L4πr2.F(r)=\frac{L}{4\pi r^2}.

The outward radiative and inward gravitational accelerations are

grad(r)=κL4πr2c,ggrav(r)=GMr2.g_{\rm rad}(r)=\frac{\kappa L}{4\pi r^2c}, \qquad g_{\rm grav}(r)=\frac{GM}{r^2}.

Setting them equal:

κLEdd4πr2c=GMr2⇒LEdd=4πGMcκ.\frac{\kappa L_{\rm Edd}}{4\pi r^2c} =\frac{GM}{r^2} \quad\Rightarrow\quad \boxed{L_{\rm Edd}=\frac{4\pi GMc}{\kappa}}.

Radius cancels because both accelerations fall as 1/r21/r^2. Treating this as one position-independent critical luminosity also requires MM and κ\kappa not to vary appreciably with position; stellar interiors generally require the local enclosed mass and local opacity.

The acceleration ratio is

gradggrav=κL4πGMc=LLEdd.\boxed{\frac{g_{\rm rad}}{g_{\rm grav}} =\frac{\kappa L}{4\pi GMc} =\frac{L}{L_{\rm Edd}}}.
  • L<LEddL<L_{\rm Edd}: radiation force is weaker than gravity.
  • L=LEddL=L_{\rm Edd}: the two balance exactly.
  • L>LEddL>L_{\rm Edd}: considering only these two forces, the net acceleration is outward.

This does not mean that every object above the limit is impossible, or that gas below it must be stationary. It is a comparison of forces under specified conditions.

7.2 Which opacity is used?

In the general formula, κ\kappa must describe radiation momentum-transfer efficiency. The familiar numerical expression assumes ordinary Thomson electron scattering in fully ionized gas.

In pure hydrogen, each proton has one associated electron and protons provide most of the mass:

ρ≃nemp,κes=neσTρ≃σTmp≃0.40 cm2 g−1.\rho\simeq n_em_p, \qquad \kappa_{\rm es}=\frac{n_e\sigma_{\rm T}}{\rho} \simeq\frac{\sigma_{\rm T}}{m_p} \simeq0.40\ {\rm cm^2\,g^{-1}}.

Hence

LEdd=4πGMmpcσT≃1.26×1038(MM⊙)erg s−1.\boxed{L_{\rm Edd} =\frac{4\pi GMm_pc}{\sigma_{\rm T}} \simeq1.26\times10^{38}\left(\frac{M}{M_\odot}\right) {\rm erg\,s^{-1}}}.

For fully ionized gas dominated by hydrogen and helium, with hydrogen mass fraction XX, the number of electrons per unit mass is approximately (1+X)/(2mp)(1+X)/(2m_p), giving

κes≃0.20(1+X) cm2 g−1.\kappa_{\rm es}\simeq0.20(1+X)\ {\rm cm^2\,g^{-1}}.

For example, X≃0.7X\simeq0.7 gives κes≃0.34 cm2 g−1\kappa_{\rm es}\simeq0.34\ {\rm cm^2\,g^{-1}}. Composition changes the numerical coefficient in the critical luminosity.

7.3 Which geometry is assumed?

The relation F=L/(4πr2)F=L/(4\pi r^2) assumes a locally spherically symmetric, radially outward radiation field. Gravity points radially inward, allowing a direct comparison.

A separate geometric assumption enters on the observational side:

Liso=4πd2fobs.L_{\rm iso}=4\pi d^2f_{\rm obs}.

This extrapolates the flux in our viewing direction to every direction. It defines isotropic-equivalent luminosity, which equals the true total luminosity only for genuinely isotropic emission.

These two appearances of 4π4\pi concern different physical questions:

  1. Does the distant flux measured in our direction represent other directions?
  2. How is the object's total luminosity distributed into the radial flux actually experienced by matter at a given location?

7.4 Why is observed luminosity not a mass measurement?

The Eddington formula gives a critical luminosity; an object need not radiate exactly at that value. Define the Eddington ratio

λ≡LbolLEdd,\lambda\equiv\frac{L_{\rm bol}}{L_{\rm Edd}},

where LbolL_{\rm bol} is the true luminosity summed over all bands. Then

M=κLbol4πGcλ.\boxed{M=\frac{\kappa L_{\rm bol}}{4\pi Gc\lambda}}.

Even with known geometry and opacity, luminosity alone cannot uniquely determine mass without λ\lambda. The same luminosity could come from a lower-mass object near its Eddington limit or a higher-mass object radiating at one tenth of its own limit.

Adding only the assumption λ≤1\lambda\leq1 gives

M≥κLbol4πGc,\boxed{M\geq\frac{\kappa L_{\rm bol}}{4\pi Gc}},

This is a conditional lower mass limit. Absorption, limited band coverage, distance, and directionality must also be addressed: the observed LXL_X does not automatically equal bolometric luminosity LbolL_{\rm bol}.

7.5 Numerical exercise: M82 X-1

Given

fX=4×10−12 erg cm−2 s−1,d≃3.6 Mpc.f_X=4\times10^{-12}\ {\rm erg\,cm^{-2}\,s^{-1}}, \qquad d\simeq3.6\ {\rm Mpc}.

using 1 pc≃3.086×1018 cm1\ {\rm pc}\simeq3.086\times10^{18}\ {\rm cm}:

d≃1.11×1025 cm,LX,iso=4πd2fX≃6.2×1039 erg s−1.d\simeq1.11\times10^{25}\ {\rm cm}, \qquad L_{X,\rm iso}=4\pi d^2f_X\simeq6.2\times10^{39}\ {\rm erg\,s^{-1}}.

Assuming isotropy, pure-hydrogen electron scattering, and Lbol≤LEddL_{\rm bol}\leq L_{\rm Edd}, the fact that Lbol≥LXL_{\rm bol}\geq L_X means the X-ray luminosity alone gives a conservative conditional lower bound:

MM⊙≳6.2×10391.26×1038≃49.\frac{M}{M_\odot}\gtrsim \frac{6.2\times10^{39}}{1.26\times10^{38}} \simeq49.

Radiation outside the X-ray band raises the bound under these assumptions. Beaming, super-Eddington emission, or altered effective opacity invalidates a direct application of it. 49M⊙49M_\odot is a model inference, not a measured mass.

Distinguish two sources: the exercise concerns M82 X-1, whereas the ULX pulsations reported by Bachetti et al. in 2014 came from M82 X-2. The latter establishes that at least some ULX accretors are neutron stars; standard Eddington reasoning cannot make every ULX a massive black hole. Bachetti et al., 2014

8. Why can strong magnetic fields reduce scattering for some photons?

8.1 Where does the cyclotron frequency come from?

For a nonrelativistic electron moving perpendicular to a background field, the Lorentz force supplies centripetal acceleration:

mev⊥2rL=ev⊥B0c.\frac{m_ev_\perp^2}{r_L}=\frac{ev_\perp B_0}{c}.

Therefore

ωB=v⊥rL=eB0mec.\boxed{\omega_B=\frac{v_\perp}{r_L}=\frac{eB_0}{m_ec}}.

This is angular frequency; the ordinary frequency is νB=ωB/(2π)\nu_B=\omega_B/(2\pi). In SI, ωB=eB0/me\omega_B=eB_0/m_e.

The background field introduces a new timescale 1/ωB1/\omega_B. Electron response therefore depends on the incident angular frequency ω\omega relative to ωB\omega_B.

8.2 Choose a geometry and write the driven equations of motion

Take

B0=B0z^,Ewave=E0cos⁡ωt x^.\mathbf B_0=B_0\hat{\mathbf z}, \qquad \mathbf E_{\rm wave}=E_0\cos\omega t\,\hat{\mathbf x}.

The wave electric field is perpendicular to the background magnetic field. Retain the background magnetic force but neglect the smaller wave magnetic force:

mev˙=−e(Ewave+v×B0c).m_e\dot{\mathbf v} =-e\left(\mathbf E_{\rm wave}+\frac{\mathbf v\times\mathbf B_0}{c}\right).

Writing a0=eE0/mea_0=eE_0/m_e, the component equations are

v˙x=−a0cos⁡ωt−ωBvy,v˙y=ωBvx.\begin{aligned} \dot v_x&=-a_0\cos\omega t-\omega_Bv_y,\\ \dot v_y&=\omega_Bv_x. \end{aligned}

The magnetic field couples motion in the two directions. We focus on the periodic response driven by the incident wave, not any preexisting free cyclotron motion.

8.3 Low-frequency picture: a transverse drift that follows the electric field

For ω≪ωB\omega\ll\omega_B, the electric field varies much more slowly than electron gyration. Electric and magnetic forces in the xx direction cancel to leading order:

−a0cos⁡ωt−ωBvy≃0.-a_0\cos\omega t-\omega_Bv_y\simeq0.

giving

vy≃−a0ωBcos⁡ωt=−cE0B0cos⁡ωt.v_y\simeq-\frac{a_0}{\omega_B}\cos\omega t =-\frac{cE_0}{B_0}\cos\omega t.

This is the E×B\mathbf E\times\mathbf B drift in this geometry. As it follows the incident electric field, it produces acceleration:

ay=v˙y≃a0ωωBsin⁡ωt.a_y=\dot v_y\simeq a_0\frac{\omega}{\omega_B}\sin\omega t.

Using v˙y=ωBvx\dot v_y=\omega_Bv_x further verifies

ax≃a0(ωωB)2cos⁡ωt.a_x\simeq a_0\left(\frac{\omega}{\omega_B}\right)^2\cos\omega t.

Thus, in the low-frequency limit, the dominant driven acceleration amplitude is

amag≃a0ωωB.\boxed{a_{\rm mag}\simeq a_0\frac{\omega}{\omega_B}}.

The key is that the magnetic field changes the electron's response and reduces its net acceleration, not that the electron stops moving entirely.

8.4 Why does the cross section decrease as the square of the acceleration?

Without a magnetic field,

⟨a2⟩0=a022.\langle a^2\rangle_0=\frac{a_0^2}{2}.

For the low-frequency transverse response in a strong field,

⟨a2⟩mag≃a022(ωωB)2.\langle a^2\rangle_{\rm mag} \simeq\frac{a_0^2}{2}\left(\frac{\omega}{\omega_B}\right)^2.

Since P∝a2P\propto a^2 and the incident flux is unchanged in this comparison,

σeffσT=⟨Pmag⟩⟨P0⟩=⟨a2⟩mag⟨a2⟩0≃(ωωB)2.\frac{\sigma_{\rm eff}}{\sigma_{\rm T}} =\frac{\langle P_{\rm mag}\rangle}{\langle P_0\rangle} =\frac{\langle a^2\rangle_{\rm mag}}{\langle a^2\rangle_0} \simeq\left(\frac{\omega}{\omega_B}\right)^2.

we obtain

σeff≃σT(ωωB)2.\boxed{\sigma_{\rm eff}\simeq\sigma_{\rm T} \left(\frac{\omega}{\omega_B}\right)^2}.

For example, if ω/ωB=0.1\omega/\omega_B=0.1, the cross section in this simplified case is about 1%1\% of the Thomson cross section.

8.5 Essential applicability conditions

  • This is a low-frequency, nonrelativistic classical-response derivation, far from cyclotron resonance.
  • If the wave electric field is parallel to the background magnetic field, electron motion along it is not magnetically constrained and does not exhibit this transverse suppression.
  • Real radiation in magnetized media includes different propagation directions and polarization modes; not all photons experience the same reduction in cross section.
  • Near ω∼ωB\omega\sim\omega_B, cyclotron resonance occurs, the low-frequency approximation fails, and scattering can be enhanced.
  • Quantitative magnetar calculations additionally require quantum effects, spectra, mode conversion, and more complete cross sections. This derivation explains the basic scaling.

In the literature, the extraordinary mode (X-mode, also called E-mode) has this suppressed scattering below the cyclotron frequency. Its wave electric field is perpendicular to the plane containing the propagation direction and background magnetic field. Mode dependence of magnetized scattering

9. Why can standard Eddington reasoning fail? Three distinct steps

The complete inference chain is

fobs→isotropyL=4πd2fobs→locally spherical propagationF(r)=L4πr2→specified opacitygrad=κF(r)c.f_{\rm obs} \xrightarrow{\text{isotropy}} L=4\pi d^2f_{\rm obs} \xrightarrow{\text{locally spherical propagation}} F(r)=\frac{L}{4\pi r^2} \xrightarrow{\text{specified opacity}} g_{\rm rad}=\frac{\kappa F(r)}{c}.

The three mechanisms modify the observational conversion, local flow geometry, and momentum-coupling efficiency, respectively.

9.1 Directional emission: bright toward us does not mean bright everywhere

A telescope measures only light directed toward us. The true total luminosity is

Ltrue=∫dLdΩ dΩ,L_{\rm true}=\int\frac{dL}{d\Omega}\,d\Omega,

whereas Liso=4πd2fobsL_{\rm iso}=4\pi d^2f_{\rm obs} assumes that every direction is as bright as ours.

In a simple model, light is uniformly concentrated within total solid angle Ω\Omega, and we lie inside it. Then

fobs=LtrueΩd2.f_{\rm obs}=\frac{L_{\rm true}}{\Omega d^2}.

Defining beaming factor b=Ω/(4π)b=\Omega/(4\pi) gives

Liso=Ltrueb,Ltrue=bLiso.\boxed{L_{\rm iso}=\frac{L_{\rm true}}b}, \qquad L_{\rm true}=bL_{\rm iso}.

For example, if b=0.1b=0.1, the isotropic-equivalent luminosity is ten times the true luminosity. With other assumptions unchanged, using LisoL_{\rm iso} as the true luminosity overestimates the associated mass estimate or conditional lower limit by tenfold.

In some ULX models, thick accretion flows and outflows form a funnel, and scattered light preferentially escapes along it. Such geometric beaming does not require a relativistic jet. King, 2009

This mechanism changes the conversion from observed flux to true luminosity. Directionality alone does not establish a numerical amplification factor; a broad pulse alone cannot rigorously exclude substantial beaming either.

9.2 Sideways leakage from an accretion column: matter goes down, energy escapes sideways

A strong magnetic field can channel accretion near a neutron star onto small areas near its magnetic poles. At higher accretion rates, a magnetically confined accretion column forms.

             Accreting matter
                    ↓
                    ↓
             ┌─────────────┐
    Light ←  │   Hot gas   │  → Light
    Light ←  │   Column    │  → Light
             └──────┬──────┘
                    ↓
             Neutron-star surface

An accretion column is not a pipe with solid walls, but a magnetically confined gas stream. Falling matter decelerates, releasing energy, heating the gas, and producing radiation.

Photons may scatter repeatedly and diffuse outward as a random walk. In a tall, narrow column with relatively small transverse optical depth, escaping sideways is easier than traveling upward through the entire stream.

Sideways escape means that most net energy leaves through the column's sides, not that every newly created photon immediately flies straight sideways.

In spherical geometry, outward light directly opposes inward matter, so radiation force resists infall. For a column, the relevant force is the component along the column opposing the inflow; not all luminosity can be assigned to that direction.

Schematically,

grad,∥≃κ∥F∥c,g_{{\rm rad},\parallel}\simeq\frac{\kappa_\parallel F_\parallel}{c},

where F∥F_\parallel is the outward flux along the column, opposing infall. Total luminosity instead includes energy leaving every column surface:

Ltrue=∫column surfaceF⋅dA.L_{\rm true}=\int_{\text{column surface}}\mathbf F\cdot d\mathbf A.

Thus, large LtrueL_{\rm true} does not require F∥=Ltrue/(4πr2)F_\parallel=L_{\rm true}/(4\pi r^2).

Also remember:

  • Transverse radiation still exerts pressure and tends to expand the column, requiring confinement by magnetic stresses.
  • Radiation force remains along the column and can form a radiation-dominated shock, decelerating gas that subsequently settles.
  • Sideways leakage does not permit unlimited luminosity. Field strength, column geometry, optical depth, and energy transport constrain the actual structure.

This mechanism supplies another route for energy to escape, helping accretion continue at high true luminosity. Accretion columns and high-luminosity models

9.3 Reduced effective opacity: the same light pushes less strongly

The preceding mechanisms change where light travels; this one changes how efficiently it transfers momentum to matter.

If a strong magnetic field suppresses scattering in the relevant modes, the effective opacity for radiation force can also decrease. In a simplified model that retains spherical symmetry,

grad=κeffFc,Lcrit=4πGMcκeff.g_{\rm rad}=\frac{\kappa_{\rm eff}F}{c}, \qquad L_{\rm crit}=\frac{4\pi GMc}{\kappa_{\rm eff}}.

As a hypothetical example, if the average effective opacity becomes 1/1001/100 of its original value, the critical luminosity in that same model increases by a factor 100100.

But a single mode's σeff/σT\sigma_{\rm eff}/\sigma_{\rm T} cannot be used as the entire star's κeff/κes\kappa_{\rm eff}/\kappa_{\rm es} without averaging over spectrum, direction, and polarization.

Two distinct meanings of direction must also be separated:

  • Sideways leakage compares light propagation direction with matter-flow direction.
  • Polarization suppression compares wave electric-field direction with background magnetic-field direction.

9.4 Comparing the three mechanisms

MechanismAssumption modifiedResult
Directionality / beamingEqual brightness in all directionsLisoL_{\rm iso} can exceed the true total luminosity
Sideways leakage from an accretion columnAll light travels radially against the accretion flowTotal luminosity is large, but the opposing radiation force does not grow according to the spherical formula
Reduced effective opacityOrdinary Thomson momentum-coupling efficiencyThe same local flux produces a smaller radiation force

All three effects can coexist. A super-Eddington equivalent luminosity alone cannot uniquely determine mass, field strength, or beaming.

10. Magnetars: magnetic fields change radiation transport and store burst energy

The magnetic field has two distinct roles:

  1. Changing photon escape: reduced opacity in some modes raises the critical luminosity under the corresponding conditions.
  2. Providing an energy reservoir: magnetic energy released through field rearrangement or decay can power bursts.

Paczyński (1992), cited in the course, connects strong fields, low scattering opacity, super-Eddington emission, and magnetic-energy budgets. This is a physical explanation of magnetar phenomena, not a unique magnetic-field measurement from luminosity alone. Paczyński, 1992

10.1 Stored energy from magnetic energy density

In Gaussian-cgs, magnetic energy density is

uB=B28π.u_B=\frac{B^2}{8\pi}.

When BB is in G, uBu_B has units erg cm−3{\rm erg\,cm^{-3}}. Internal magnetic energy is generally

EB=∫VB(r)28π dV.E_B=\int_V\frac{B(\mathbf r)^2}{8\pi}\,dV.

For an order-of-magnitude estimate with approximately uniform internal field strength:

EB≃B28π4πR33=B2R36.E_B\simeq\frac{B^2}{8\pi}\frac{4\pi R^3}{3} =\boxed{\frac{B^2R^3}{6}}.

The coefficient 1/61/6 is the product of 1/(8π)1/(8\pi) from energy density and 4π/34\pi/3 from spherical volume.

10.2 Typical magnetar scales

Take B=1015 GB=10^{15}\ {\rm G} and R=10 km=106 cmR=10\ {\rm km}=10^6\ {\rm cm}:

EB≃(1015)2(106)36=10486≃1.7×1047 erg.E_B\simeq\frac{(10^{15})^2(10^6)^3}{6} =\frac{10^{48}}6 \simeq1.7\times10^{47}\ {\rm erg}.

Therefore

EB≃1.7×1047(B1015 G)2(R10 km)3erg.\boxed{E_B\simeq1.7\times10^{47} \left(\frac{B}{10^{15}\ {\rm G}}\right)^2 \left(\frac{R}{10\ {\rm km}}\right)^3 {\rm erg}}.

A tenfold increase in field strength increases stored energy a hundredfold; doubling the radius increases it eightfold.

10.3 Required field strength from burst energy

If only a fraction η\eta of the internal magnetic energy becomes radiation in the burst, we require

ηEB≳Eburst.\eta E_B\gtrsim E_{\rm burst}.

Therefore

B≳6EburstηR3.\boxed{B\gtrsim\sqrt{\frac{6E_{\rm burst}}{\eta R^3}}}.

For example, with Eburst=1045 ergE_{\rm burst}=10^{45}\ {\rm erg} and R=10 kmR=10\ {\rm km}:

B≳7.7×1013η−1/2 G.B\gtrsim7.7\times10^{13}\eta^{-1/2}\ {\rm G}.

If η=0.01\eta=0.01, the required field is approximately 7.7×1014 G7.7\times10^{14}\ {\rm G}.

10.4 What does BB represent in this estimate?

More precisely, define the internal volume-rms field strength

Brms=1V∫VB2 dV.B_{\rm rms}=\sqrt{\frac1V\int_V B^2\,dV}.

For a spherical integration volume, replacing BB by BrmsB_{\rm rms} gives internal magnetic energy Brms2R3/6B_{\rm rms}^2R^3/6 without requiring an everywhere uniform field.

However, BrmsB_{\rm rms} need not equal the surface dipole field inferred from spin-down or other observations. Total magnetic energy is not all releasable in a single event: the release fraction depends on field structure and evolution. This estimate concerns internal energy only; the external magnetosphere may store additional energy.

11. Review priorities: what to remember and what to derive

These priorities support understanding this lecture and solving problems independently. They are not an additional instructor-issued exam syllabus.

11.1 Basic formulas: know the symbols, dimensions, and assumptions

FormulaPhysical meaning and conditions
pγ=Eγ/cp_\gamma=E_\gamma/cLight carries momentum and can exert force on matter
F=q(E+v×B/c)\mathbf F=q(\mathbf E+\mathbf v\times\mathbf B/c)Electromagnetic force on a charge; cgs here
S=cE×B/(4π)\mathbf S=c\mathbf E\times\mathbf B/(4\pi)Magnitude and direction of electromagnetic energy flow
uEM=(E2+B2)/(8π)u_{\rm EM}=(E^2+B^2)/(8\pi)Field energy density
P=2q2a2/(3c3)P=2q^2a^2/(3c^3)Larmor power of a nonrelativistically accelerated charge
g=GM/r2g=GM/r^2Newtonian gravitational acceleration
E=BE=BVacuum plane wave in cgs; not valid for arbitrary electromagnetic fields
⟨cos⁡2ωt⟩=1/2\langle\cos^2\omega t\rangle=1/2Cycle average of a sinusoidal oscillation

These can serve as starting points in problems without rederiving Maxwell's equations each time. Although the Larmor formula may be used directly, its derivation by integrating the far field is worth mastering.

11.2 Definitions: know exactly what is being defined

DefinitionCommon confusion
σ=⟨Psc⟩/⟨Finc⟩\sigma=\langle P_{\rm sc}\rangle/\langle F_{\rm inc}\rangleEffective, not necessarily geometric area; do not mix mean and peak values
κ=nσ/ρ\kappa=n\sigma/\rhoConverts a single-particle cross section into interaction capacity per unit mass; combine processes appropriately
dτ=κρ dsd\tau=\kappa\rho\,dsDimensionless optical depth
re=e2/(mec2)r_e=e^2/(m_ec^2)Classical electromagnetic length scale, not the electron's physical radius
Liso=4πd2fobsL_{\rm iso}=4\pi d^2f_{\rm obs}Isotropic-equivalent luminosity, not automatically the true luminosity
λ=Lbol/LEdd\lambda=L_{\rm bol}/L_{\rm Edd}Eddington ratio, not necessarily unity

A definition is not a theorem requiring proof. Understand why it is useful and when it can be identified with a physical quantity.

11.3 Core results: reconstruct the derivations without the notes

Mean incident flux

S=c4πE×B⟶F(t)=cE024πcos⁡2ωt⟶⟨F⟩=cE028π.\mathbf S=\frac c{4\pi}\mathbf E\times\mathbf B \longrightarrow F(t)=\frac{cE_0^2}{4\pi}\cos^2\omega t \longrightarrow\langle F\rangle=\frac{cE_0^2}{8\pi}.

Focus on the origin of 1/21/2 and the distinction between E0E_0 and ErmsE_{\rm rms}.

Thomson cross section

a0=eE0me⟶⟨P⟩=2e23c3⟨a2⟩⟶σT=⟨P⟩⟨F⟩=8π3re2.a_0=\frac{eE_0}{m_e} \longrightarrow\langle P\rangle=\frac{2e^2}{3c^3}\langle a^2\rangle \longrightarrow\sigma_{\rm T}=\frac{\langle P\rangle}{\langle F\rangle} =\frac{8\pi}{3}r_e^2.

Focus on consistent averaging and why field strength and frequency cancel. The commonly used σT≃6.65×10−25 cm2\sigma_{\rm T}\simeq6.65\times10^{-25}\ {\rm cm^2} is worth memorizing; the exact numerical value of rer_e has slightly lower priority.

Radiative acceleration and Eddington luminosity

Intercepted light energy⟶Transferred momentum⟶grad=κFc⟶F=L4πr2⟶grad=GMr2.\text{Intercepted light energy} \longrightarrow\text{Transferred momentum} \longrightarrow g_{\rm rad}=\frac{\kappa F}{c} \longrightarrow F=\frac{L}{4\pi r^2} \longrightarrow g_{\rm rad}=\frac{GM}{r^2}.

Focus on each step's geometric, opacity, and force-balance assumptions. The result is a critical luminosity; inferring mass additionally requires the Eddington ratio, true bolometric luminosity, and observational conversion.

Scattering suppression in a strong magnetic field

ωB=eB0mec,amag∼a0ωωB⟶P∝a2⟶σeff∼σT(ωωB)2.\omega_B=\frac{eB_0}{m_ec}, \qquad a_{\rm mag}\sim a_0\frac{\omega}{\omega_B} \longrightarrow P\propto a^2 \longrightarrow\sigma_{\rm eff}\sim\sigma_{\rm T} \left(\frac{\omega}{\omega_B}\right)^2.

Do not merely memorize the squared scaling: understand that it follows from acceleration suppression and applies only to the appropriate frequency, polarization, and approximations. Reconstruct the two coupled velocity equations rather than memorizing a complicated general solution.

Magnetic-energy estimates

EB=∫B28π dV⟶EB∼B2R36⟶B≳6EburstηR3.E_B=\int\frac{B^2}{8\pi}\,dV \longrightarrow E_B\sim\frac{B^2R^3}{6} \longrightarrow B\gtrsim\sqrt{\frac{6E_{\rm burst}}{\eta R^3}}.

Reconstruct the coefficient as density times volume, explain that the field is an internal rms value, and note that release efficiency need not be unity.

11.4 Deeper electrodynamics: understand the starting point and subsequent steps

Obtaining Erad=∣q∣asin⁡θ/(c2r)E_{\rm rad}=|q|a\sin\theta/(c^2r) from Maxwell's equations or retarded potentials requires fuller electrodynamics. For now it can be taken as input, but you should then be able to complete

Erad⟶S∝Erad2⟶P=∫Sr2 dΩ.E_{\rm rad}\longrightarrow S\propto E_{\rm rad}^2 \longrightarrow P=\int Sr^2\,d\Omega.

This explains the Larmor angular pattern and coefficient 2/32/3 instead of merely memorizing them.

11.5 Self-test questions

  1. Can you derive σT\sigma_{\rm T} from the incident electric field without forgetting time averaging?
  2. Why does obtaining 16π/316\pi/3 often signal mixed peak and mean quantities?
  3. Why does grad=κF/cg_{\rm rad}=\kappa F/c have dimensions of acceleration rather than force?
  4. Why does r2r^2 cancel in the Eddington derivation? How should MM and κ\kappa be interpreted inside a star?
  5. What distinguishes LisoL_{\rm iso}, LtrueL_{\rm true}, LXL_X, and LbolL_{\rm bol}?
  6. Why does assuming only Lbol≤LEddL_{\rm bol}\leq L_{\rm Edd} give a lower mass bound?
  7. Which inference step is changed by beaming, sideways leakage, and reduced opacity, respectively?
  8. Why is the transverse scattering-suppression formula inapplicable when the wave electric field is parallel to the background field?
  9. Does sideways-escaping light still exert force on gas? Why does an accretion column require magnetic confinement?
  10. Which energy-budget assumptions are needed to infer a magnetic field from a burst energy?

12. Formula reference and sources

12.1 Formula reference (Gaussian-cgs)

TopicFormulaConditions or explanation
Mean wave flux⟨F⟩=cE02/(8π)\langle F\rangle=cE_0^2/(8\pi)Sinusoidal vacuum plane wave; E0E_0 is the peak amplitude
Radiated powerP=2q2a2/(3c3)P=2q^2a^2/(3c^3)Instantaneous nonrelativistic Larmor power
Thomson cross sectionσT=8πre2/3\sigma_{\rm T}=8\pi r_e^2/3Free, nonrelativistic electrons with negligible recoil
Classical electron radiusre=e2/(mec2)r_e=e^2/(m_ec^2)Defined electromagnetic length scale
Radiative accelerationgrad=κFF/cg_{\rm rad}=\kappa_FF/cUse a mean opacity appropriate to radiation force
Eddington luminosityLEdd=4πGMc/κL_{\rm Edd}=4\pi GMc/\kappaComparison of spherical radial radiation and gravity
Electron-scattering opacityκes≃0.20(1+X) cm2 g−1\kappa_{\rm es}\simeq0.20(1+X)\ {\rm cm^2\,g^{-1}}Fully ionized gas dominated by hydrogen and helium
Cyclotron angular frequencyωB=eB0/(mec)\omega_B=eB_0/(m_ec)Nonrelativistic electrons
Low-frequency cross-section suppressionσeff∼σT(ω/ωB)2\sigma_{\rm eff}\sim\sigma_{\rm T}(\omega/\omega_B)^2Appropriate transverse mode, ω≪ωB\omega\ll\omega_B
Simple beaming modelLiso=Ltrue/bL_{\rm iso}=L_{\rm true}/bLight uniformly confined to solid angle 4πb4\pi b, with the observer inside it
Internal magnetic energyEB=Brms2R3/6E_B=B_{\rm rms}^2R^3/6Spherical integration volume of radius RR

12.2 References