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Airfoil 204 x 90 Mesh Images
Updated 4/22/08
Compressible flows utilizing the noslip boundary condition are still being tested.
Currently, I am only looking at the qualitative aspects of these results.
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Density at 60.0 seconds 2000 steps
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Pressure at 60.0 seconds 2000 steps
Go here to see video.
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Mach Number at 60.0 seconds 2000 steps
Go here to see video.
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