Approximate Crank–Nicolson Algorithm with Higher-Order PML Implementation for Plasma Simulation in Open Region Problems

<div>The RCS of the flight vehicle model versus frequency with plasma sheath obtained by (a) FDTD-PML, CNDS-PML, CNAFS-PML, HO-PML, and CNDS-HO-PML CFLN = 1; (b) CNDS-PML, CNAFS-PML, and CNDS-HO-PML CFLN = 10.</div>

International Journal of Antennas and Propagation

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Figure 4

Figure 4: Approximate Crank–Nicolson Algorithm with Higher-Order PML Implementation for Plasma Simulation in Open Region Problems 