1 / 17

Shock Acceleration at an Interplanetary Shock: A Focused Transport Approach

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 ).

shanta
Télécharger la présentation

Shock Acceleration at an Interplanetary Shock: A Focused Transport Approach

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Shock Acceleration at an Interplanetary Shock:A Focused Transport Approach J. A. le Roux Institute of Geophysics & Planetary Physics University of California at Riverside

  2. 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 where

  3. Transform (p||, p’)(’, M) where Conservation of magnetic moment Electric field drift Grad-B drift Curvature drift

  4. 2. The Focused Transport Equation for f(x,p’,’,t) To get focused transport equation, assume in guiding center kinetic equation E = -U B, wherebyVE = U Transform parallel momentum to moving frame (p|| = p’|| + mU||) Transform (p’||,p’)  (p’, ’ ) Convection Mirroring/focusing Adiabatic energy changes Parallel Diffusion

  5. 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

  6. 3. Results: (a) Proton spectra in SW frame SW Kappa distribution( = 3)  1/r2 SW density = C 1 AU 0.7 AU f(v)  v-3.2 f(v)  v-4.2 f(v)  v-3.7 upstream downstream SW density  1/r2

  7. SW Kappa distribution( = 3)  1/r2 __0.13 AU Shift in peak to lower energies ---0.27 AU …0.49 AU f(v)  v-5.3 _.._0.71 AU ___1 AU f(v)  v-32

  8. (b) Anisotropies in SW frame at 1 AU downstream shock =25% upstream =82% 100 keV 1 MeV =9% 10 MeV

  9. (c) Spatial distributions across shock 100 keV 100 MeV 1 MeV 10 MeV

  10. (d) Time distributions at 1 AU 10 MeV 10 MeV 100 keV 100 MeV

  11. 3. COMPARISON OF STRONG AND WEAK SHOCKS: (a) Accelerated spectra f(v)  v-3.7 Weak shock (s=3.32.2) Strong shock (s=4) f(v)  v-7.1 0.7 AU 0.7 AU Spectrum harder than predicted by steady state DSA Spectrum softer than predicted by steady state DSA

  12. (b) Anisotropies Strong shock(s=4) Weak shock(s=3.32.2) 100 keV 100 keV Pitch-angle anisotropy larger for a strong shock

  13. 1D parallel Alfven wave transport equation at parallel shock solved Convection Convection in wave number space- Compression shortens wave length Compression raises wave amplitude Wave generation by SEP anisotropy Wave-wave interaction – forward cascade in wave number space in inertial range

  14. Wave-wave interaction Model (Zhou & Matthaeus, 1990): • 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 energyconservation in 3-wave coupling does not hold Kraichnan cascade I(k)  k-3/2 tA << tNL(U = VA << VA) or (B << Bo) • Kolmogorov cascade I(k)  k-5/3 tNL << tA (U = VA >> VA) or (B >> Bo) Comments

  15. Alfven wave Spectrum (Kolmogorov Cascade) downstream NeedCK > 8 for cascading to work at shock at 0.1 AU upstream 0.3 AU 0.5 AU 0.7 AU 1 AU

  16. 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 kminfor 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 rateat 1 AU

  17. A Weak Kinetic Turbulence Theory Approach to Wave Cascading? Nonlinear wave-wave interaction Wave Kinetic Equation Wave generation Wave decay Linear wave-particle interaction Wave-wave interaction term a Boltzmann scattering term When assume weak scattering, term can be put in Fokker-Planck form so that nonlinear diffusion coefficients for wave cascading Dkk can be derived

More Related