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Table 1.

Parameters of numerical calculations.

Model Γ R0 s g
(104) (102 G) (1047 s−1) (cm)
C1R14Γ240 240 2 2 4 1014
C1R15Γ120 120 10 1 16 1015
C2R14Γ240 240 2 2 64 1014
C2R15Γ460 460 5 1 2 1015
C3R14Γ1900 1900 1.4 3 1.2 1014
C3R15Γ1900 1900 1.4 3 1.2 1015
C4R14Γ460 460 5 0.8 4 1014
AR14Γ200 200 3.5 0.6 20 1014 0.35
AR14Γ150 150 3.5 0.6 20 1014 0.55
A14Γ80 80 3.5 1.0 80 1014 1.0
AR15Γ230 230 5 2 8 1015 1.0
AG1R14Γ300 300 4.5 0.6 32 1014 0.0 0.7
AG214Γ150 150 5.0 0.6 20 1014 0.55 0.5
AG1R15Γ250 250 5 2 8 1015 0.0 1.0
AG2R15Γ230 230 5 2 8 1015 1.0 1.0

Notes. Three distinct groups of cases are listed. In the fist group, letter C in the model name denotes that the shell is moving at a constant Lorentz factor, the numbers (1–4) signify that the cooling process is dominated by synchrotron cooling, SSC cooling, adiabatic cooling, or SSC+adiabatic cooling, respectively. In the second group, letter A denotes that the shell is moving at an increasing Lorentz factor, and s here describes the index of bulk acceleration law. In the third group, the letter G means that a broken power-law profile of is considered, while the acceleration effect is also taken into account (letter A). The index g describes the evolution of , which could refer to Eq. (5).

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