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The flow through a transonic fan rotor (designated rotor 37 by
NASA Lewis) was computed. It has 36 blades. The calculation was
performed at a rotational speed of 17189 rpm. The domain boundaries
consist of a hub, blade and shroud surface, a pressure inlet and
outlet surface, and periodic surfaces.
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Number of cells
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89,856
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Cell type
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hexahedral
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Models
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k-epsilon turbulence
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Solver
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coupled implicit
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Plots
- Serial
- Parallel
Results
In the table below, a rating
listed in red corresponds to the redzone result, and one in bold is a peak result. Bold
red is used to indicate that the run was both the peak
and redzone result.
Results are listed alphabetically by platform, within each FLUENT version.
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