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SINGULARLY PERTURBED CONVECTION-DIFFUSION BOUNDARY-VALUE PROBLEMS USING ADAPTIVE GRID

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Figure 2.1: Shishkin mesh with N = 8 for left layer.
Figure 2.3(a) represents the movement of mesh after each iteration and Figure 2.3(b) shows the final computed mesh corresponding to the solution of Example 2.6.1
Figure 2.3: Movements of mesh towards left with ε = 1e − 2 and N = 20 for Example 2.6.1.
Figure 2.5: Normalized flux and the error in the normalized flux for Example 2.6.2 with ε = 1e − 2 and N = 32.
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