Fig. 4

Convergence history of the four components of the
source vector
for x = 0 and μ = 0.025 calculated with the
core-wing method. Same model as in Fig. 3. The
dotted lines show the initial solutions (ϵB for
, and zero for
all other components). Since the slab is symmetric about the mid-plane, the results
are shown only for a half-slab,
τ ∈ [0,T/2] .
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