13 lines
417 B
Plaintext
13 lines
417 B
Plaintext
nacaAirfoil
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* large domain with airfoil section near centre
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* extremely non-orthogonal, highly skew mesh refined around the airfoil
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* running at Mach 1.78
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* limited 0.5 on all laplacianSchemes because the mesh is so poor
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* run to t = 0.02 with nextWrite; change to stopAt endTime to continue running
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* deltaT can be increased later in the run to 2e-07
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prism
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~~~~~
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* run to t = 0.0014 for convergence
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