Shock Acceleration at an Interplanetary Shock: A Focused Transport Approach J. A. le Roux Institute of Geophysics & Planetary Physics University of California at Riverside 1. The Guiding center Kinetic Equation for f(x,p||,p’,t) Transform position x to guiding center position xg (x = xg+rg) Transform transverse momentum to plasma frame p = p’ + VE Smallness parameter = m/q << 1 (small gyroradius, large gyrofrequency) Keep terms to order o Average over gyrophase dp|| f f Vg t x g dt dp' f p|| dt f f p' t c where Vg v||b VE , dp|| dt dp ' dt qE|| 1 p' v' dB || B mVE , 2 B dt 1 p||v ' 1 || B p ' VE b ||VE 2 B 2 Transform (p||, p’)(’, M) f f dM f d ' Vg1 t x g dt M dt f f ' t c where Vg1 v||b VE , dM 0, dt d ' B qE Vg2 M , dt t Vg2 v||b VE Conservation of magnetic moment M b || M B 2 B mb d v||b q q B qB dt Electric field drift Grad-B drift Curvature drift 2. The Focused Transport Equation for f(x,p’,’,t) To get focused transport equation, assume in guiding center kinetic equation E = -U B, whereby VE = U Transform parallel momentum to moving frame (p|| = p’|| + mU||) Transform (p’||,p’) (p’, ’ ) f f U i vbi t xi bi f U i U i 2 dU i 2q 1 2 1 v 3bi b j bi Ei bi 2 x x x v dt p i i j 1 f U U i dU i 1 q 1 2 i 1 3 2 bi b j bi Ei bi p xi 2 x j v dt p 2 p f D QPUI Convection Mirroring/focusing Adiabatic energy changes Parallel Diffusion Advantages Same mechanisms as standard cosmic-ray transport equation No restriction on pitch-angle anisotropy - injection Describe both (i) 1st order Fermi, and (ii) shock drift acceleration with or without scattering Disadvantages No cross-field diffusion Gradient and curvature drift effect on spatial convection ignored Magnetic moment conservation at shocks 3. Results: (a) Proton spectra in SW frame SW Kappa distribution ( = 3) 1/r2 1012 1011 1010 1098 107 106 105 104 103 102 101 100 10-1 10-2 10-3 10-4 10 10-1 upstream 1 AU f(v) v-3.2 100 101 v/Ue 102 downstream 103 f(v)(s3/km6) f(v)(s3/km6) SW density = C 1013 1012 1011 1010 1098 107 106 105 104 103 102 101 100 10-1 10-2 10-3 10 10-1 0.7 AU f(v) v-4.2 f(v) v-3.7 100 101 v/Ue SW density 1/r2 102 103 SW Kappa distribution ( = 3) 1/r2 ---0.27 AU …0.49 AU _.._0.71 AU ___1 AU f(v)(s3/km6) __0.13 AU 1012 1011 1010 1098 107 106 105 104 103 102 101 100 10-1 10-2 10-3 10-4 10 10-1 Shift in peak to lower energies f(v) v-5.3 100 101 v/Ue 102 f(v) v-32 103 (b) Anisotropies in SW frame at 1 AU downstream 1.00 1.0 upstream 0.10 =82% =25% f() f() shock 100 keV 1 MeV 0.01 -1 0 1 -1 0 1.00 f() =9% 10 MeV 0.10 -1 0.1 0 1 1 (c) Spatial distributions across shock 104 103 100 keV f(z) 102 101 100 10-1 100 MeV 10-2 0.5 1 MeV 1.0 z(AU) 1.5 10 MeV (d) Time distributions at 1 AU 102 101 f(t) 10 MeV 100 10-1 10 MeV 10-2 100 keV 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 t(hours) 100 MeV 3. COMPARISON OF STRONG AND WEAK SHOCKS: (a) Accelerated spectra f(v) v-3.7 1013 1012 1011 1010 1098 107 106 105 104 103 102 101 100 10-1 10-2 10-3 10 0.7 AU 10-1 100 Weak shock (s=3.32.2) f(v)(s3/km6) f(v)(s3/km6) Strong shock (s=4) 101 102 v/Ue Spectrum harder than predicted by steady state DSA 103 1013 1012 1011 1010 1098 107 106 105 104 103 102 101 100 10-1 10-2 10-3 10 10-1 f(v) v-7.1 0.7 AU 100 101 102 v/Ue Spectrum softer than predicted by steady state DSA 103 (b) Anisotropies Strong shock (s=4) Weak shock (s=3.32.2) 100 f() f() 100 10-1 10-1 100 keV 100 keV 10-2 -1 0 1 10-2 -1 0 Pitch-angle anisotropy larger for a strong shock 1 1D parallel Alfven wave transport equation at parallel shock solved I t U sh V A I z U sh V A k I z k 1 U sh I 2 z (ki ) I I Dkk ( I ( k ), k ) k k Convection Convection in wave number spaceCompression shortens wave length Compression raises wave amplitude Wave generation by SEP anisotropy Wave-wave interaction – forward cascade in wave number space in inertial range Wave-wave interaction Model (Zhou & Matthaeus, 1990): k2 Dkk ts • Kolmogorov cascade I(k) k-5/3 tNL << tA (U = VA >> VA ) or (B >> Bo) t s t NL l U Kraichnan cascade I(k) k-3/2 tA << tNL (U = VA << VA ) or (B << Bo) ts t A l VA Comments • Turbulence can be modeled as a nonlinear diffusion process in wavenumber space (Dkk) • Ad-hoc turbulence model based on dimensional analysis • Contrary to weak turbulence theory – assume that 3-wave coupling for Alfven waves is possible – imply wave resonance broadening – momentum and energy conservation in 3-wave coupling does not hold I(k||)(eVcm-2) Alfven wave Spectrum (Kolmogorov Cascade) 1016 1015 1014 1013 1012 1011 1010 109 108 107 106 105 104 103 downstream at shock at 0.1 AU upstream 0.3 AU 0.5 AU 0.7 AU 1 AU 101 102 103 104 105 106 107 k||re Need CK > 8 for cascading to work Kolmogorov or Kraichnan Cascade? Bastille Day CME event Kallenbach, Bamert, le Roux et al., 2008 Used Marty Lee (1983) quasi-linear theory extended to include nonlinear wave cascading via a diffusion term in wavenumber space. Applied theory to Bastille Day and Halloween #1 CME events to calculate kmin for wave growth Find that Kraichnan-type turbulence gives the correct kmin Kolmogorov-type turbulence overestimates kmin by a factor 2-4 Halloween CME event #1 Vasquez et al. , 2007 For cascade rates and proton heating rates to agree in SW – CK= 12 needed instead of the expected CK ~1 Kraichnan cascade rate is close to heating rate at 1 AU A Weak Kinetic Turbulence Theory Approach to Wave Cascading? Nonlinear wave-wave interaction Wave Kinetic Equation dI ( k ) 2 ( k ) I ( k ) dk '[| a k ,k ' |2 I ( k ' ) I ( k ' ' ) 2a k ,k ' a k ',k I ( k ) I ( k ' ' )] ( ( k ) ( k ' ) ( k ' ' )) dt Linear waveparticle interaction Wave generation Wave decay Wave-wave interaction term a Boltzmann scattering term When assume weak scattering, term can be put in FokkerPlanck form so that nonlinear diffusion coefficients for wave cascading Dkk can be derived
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