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Old   March 14, 2007, 12:31
Default turbomachinery
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Hi. Does anyone can advise how to define the solution domain for rotor and stator blades of a steam turbine with different number of rotor and stator blades. That means we don't have same number of channels in the rotor and stator and repeatability is only on 360 deg. So to solve only a section is a problem. We can't use cyclic boundaries where they are not.

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