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Chapter 6 Shocks & Turbulence: Comparator & Boundaries


I. Abstract & Scope
This chapter serves as the comparator/boundary layer. It packages diffusive shock acceleration (DSA) and second-order turbulent acceleration into a unified form, establishes equivalence/degeneration conditions against the reconnection/shear channels, and provides actionable discrimination criteria. Equations use English notation with backticks; SI units are used; composite expressions are parenthesized.

II. Dependencies & References

III. Normative Anchors (added in this chapter, S45-*)

IV. Body Structure


I. Comparator Models & Boundaries


II. Key Equations & Derivations (S-series)


III. Methods & Flows (M-series)


IV. Cross-References within/beyond this Volume


V. Validation, Criteria & Counterexamples

  1. Positive criteria:
    • Shock-dominant: A_dsa(E) increases with Delta_u; spectrum hardens where tau_dsa(E) < tau_loss(E) and is sensitive to r; polarization angle often steps.
    • Turbulence-dominant: timing statistics show slow variation with random walk; A_turb(E) scales with ( u_turb / c_ref )^2; polarization coherence decreases.
  2. Negative criteria:
    • If Delta_u → 0 or u_turb → 0 and fit quality does not degrade, the respective comparator channel is falsified or nonessential.
    • If setting A_dsa or A_turb to zero yields evidence ratio K ≥ 1, the comparator channel is unsupported by data.
  3. Contrasts: With A_loss(E) fixed, compare {only DSA, only turbulence, reconnection+shear, full} configurations and report spectral/timing/polarimetric signatures.

VI. Summary & Handoff
This chapter finalizes comparator packaging for shocks and turbulence, establishes equivalence/degeneration with reconnection/shear, and provides procedural extraction of dominant energy bands. Chapter 7 builds on this to deliver closed or semi-closed solutions for energy gain and spectrum formation with observational mappings.

V. Figures & Tables (this chapter)

Symbol

Meaning

Unit

Validity(Ch.)

Notes

u1, u2

upstream/downstream speed

m·s^-1

Ch.6

shock frame

r

compression ratio u1/u2

1

Ch.6

>1

Delta_u

velocity jump

m·s^-1

Ch.6

u1 - u2

delta_shock

shock thickness

m

Ch.6

normal

C_dsa

DSA time constant

1

Ch.6

>0

g_dsa(r)

per-cycle gain (DSA)

1

Ch.6

∈(0,1)

tau_dsa(E)

DSA cycle time

s

Ch.6

C_dsa D / Delta_u^2

A_dsa(E)

DSA acceleration rate

s^-1

Ch.6

g_dsa / tau_dsa

u_turb

turbulent speed

m·s^-1

Ch.6

rms

L_corr

correlation length

m

Ch.6

tau_corr

correlation time

s

Ch.6

k2

turbulent gain coeff.

1

Ch.6

>0

Phi_turb

turb. geometry/aniso factor

1

Ch.6

(0,1]

tau_turb(E)

turbulence cycle time

s

Ch.6

tau_corr + tau_sc_turb

g_turb(E)

per-cycle gain (turb.)

1

Ch.6

k2 (u_turb/c_ref)^2 Phi_turb

A_turb(E)

turbulence acceleration rate

s^-1

Ch.6

g_turb / tau_turb

eta_dom(E)

dominance factor

1

Ch.6–8

≥eta_* ⇒ dominant

Criterion

DSA

Turbulence

Shear/Reconnection mapping

Timescale

tau_dsa ∝ D/Delta_u^2

tau_turb = tau_corr + tau_sc

tau_shear ~ L_grad/Delta_u; tau_rec ~ L_cross/u_in

Gain law

g_dsa = C_g(r)

∝ (u_turb/c_ref)^2

see Ch.4/Ch.5

Polarization

step-like changes

reduced coherence

shear: smooth drift; reconnection: rapid changes

Discriminator

sensitive to r, Delta_u

sensitive to u_turb, L_corr

see Ch.4/Ch.5

Path/Measure

Form A

Form B

delta_form

gamma(ell), d ell

T_arr = ( 1 / c_ref ) * ( ∫ n_eff d ell )

T_arr = ( ∫ ( n_eff / c_ref ) d ell )

A/B


Copyright & License (CC BY 4.0)

Copyright: Unless otherwise noted, the copyright of “Energy Filament Theory” (text, charts, illustrations, symbols, and formulas) belongs to the author “Guanglin Tu”.
License: This work is licensed under the Creative Commons Attribution 4.0 International (CC BY 4.0). You may copy, redistribute, excerpt, adapt, and share for commercial or non‑commercial purposes with proper attribution.
Suggested attribution: Author: “Guanglin Tu”; Work: “Energy Filament Theory”; Source: energyfilament.org; License: CC BY 4.0.

First published: 2025-11-11|Current version:v5.1
License link:https://creativecommons.org/licenses/by/4.0/