Using Computational Fluid Dynamics for Aerodynamics
2001), which has demonstrated “text book” multigrid convergence (in 5 cycles), two-dimensional calculations of this kind can be completed in 0.5 seconds on a laptop computer (with a 2Ghz processor). A three dimensional simulation of the transonic flow over a swept wing on a 192x32x32 mesh (196,608 cells) takes 18 seconds on the same laptop.
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