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DICTIONARY OF GEOPHYSICS, ASTROPHYSICS, and ASTRONOMY

DICTIONARY OF GEOPHYSICS, ASTROPHYSICS, and ASTRONOMY

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Rρ = (β∂S/∂z)/(α∂/∂z) >1 (<strong>and</strong> stability<br />

N 2 > 0).<br />

diffusive shock acceleration Acceleration<br />

due to repeated reflection of particles in the plasmas<br />

converging at the shock front, also called<br />

Fermi-acceleration. Diffusive shock acceleration<br />

is the dominant acceleration mechanism at<br />

quasi-parallel shocks because here the electric<br />

induction field in the shock front is small, <strong>and</strong><br />

therefore shock drift acceleration is inefficient.<br />

In diffusive shock acceleration, the scattering<br />

on both sides of the shock front is the crucial<br />

process. This scattering occurs at scatter centers<br />

frozen-in into the plasma, thus particle scattering<br />

back <strong>and</strong> forth across the shock can be<br />

understood as repeated reflection between converging<br />

scattering centers (first order Fermi acceleration).<br />

Particle trajectory in diffusive shock acceleration.<br />

With f being the phase space density, U the<br />

plasma bulk speed, D the diffusion tensor, p<br />

the particle momentum, <strong>and</strong> T a loss time, the<br />

transport equation for diffusive shock acceleration<br />

can be written as<br />

∂f<br />

∂t<br />

∇U ∂f f<br />

+ U∇f −∇(D∇f)− p +<br />

3 ∂p T<br />

+ 1<br />

p 2<br />

<br />

∂<br />

p<br />

∂p<br />

2<br />

<br />

dp<br />

f = Q(r,p,t)<br />

dt<br />

with Q(r,p,t) describing an injection into the<br />

acceleration process. The terms from left to<br />

right give the convection of particles with the<br />

plasma flow, spatial diffusion, diffusion in momentum<br />

space (acceleration), losses due to particle<br />

escape from the acceleration site, <strong>and</strong> convection<br />

in momentum space due to processes<br />

that affect all particles, such as ionization or<br />

Coulomb losses.<br />

© 2001 by CRC Press LLC<br />

diffusive shock acceleration<br />

In a first-order approximation, the last two<br />

terms on the right-h<strong>and</strong> side (losses from the<br />

acceleration site <strong>and</strong> convection in momentum<br />

space) can be neglected. In addition, if we limit<br />

ourselves to steady state, some predictions can<br />

be made from this equation:<br />

1. Characteristic acceleration time. With the<br />

indices u <strong>and</strong> d denoting the properties of the<br />

upstream <strong>and</strong> downstream medium, the time required<br />

to accelerate particles from momentum<br />

po to p can be written as<br />

t =<br />

3<br />

p<br />

uu − ud<br />

po<br />

dp<br />

p ·<br />

<br />

D u<br />

+<br />

u u<br />

Dd<br />

<br />

.<br />

u d<br />

Here D denotes the diffusion coefficient. Alternatively,<br />

a characteristic acceleration time τ a<br />

can be given as<br />

τ a = 3r D u<br />

r − 1 u2 u<br />

with r = u u/ud being the ratio of the flow<br />

speeds in the shock rest frame. For a parallel<br />

shock, r equals the compression ratio. τ a then<br />

gives the time the shock needs to increase the<br />

particle momentum by a factor of e. Note that<br />

here the properties of the downstream medium<br />

have been neglected: It is tacitly assumed that<br />

the passage of the shock has created so much turbulence<br />

in the downstream medium that scattering<br />

is very strong <strong>and</strong> therefore the term D d/ud<br />

is small compared to the term D u/u u.<br />

2. Energy spectrum. In steady state, diffusive<br />

shock acceleration leads to a power law spectrum<br />

in energy J(E) = Jo · E −γ . Here the<br />

spectral index γ depends on the ratio r = u u/ud<br />

of the flow speeds only:<br />

γ = 1 r + 2<br />

2 r − 1<br />

in the non-relativistic case, or γ rel = 2γ in the<br />

relativistic case.<br />

3. Intensity increase upstream of the shock.<br />

The spatial variation of the intensity around the<br />

shock front can be described as<br />

f(x,p)= f(x,0) exp{−β|x|}<br />

with β = u u/D u. Ifβ is spatially constant, an<br />

exponential intensity increase towards the shock

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