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June 2, 2012, 04:13 |
Computational domain for a blade cascade
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#1 |
New Member
Alessio
Join Date: May 2012
Posts: 9
Rep Power: 14 |
Hello everybody,
I am going to analyze the flow within a compressor blade passage and I know about the possibility to study a single blade, and then applying the periodic boundaries to the upper and lower side of the domain. My questions are: - which are the shapes of the surfaces on which I have to apply the periodicity? - how are these shapes affecting the results, i.e. how is the periodicity acting at the interfaces? I attach a picture of a domain corresponding to my blade geometry that I found on some articles. Thanks in advance for any help! |
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June 2, 2012, 07:28 |
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#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,871
Rep Power: 144 |
Ideally the shape of the periodic boundary does not affect the results. There are a few pitfalls to avoid - like it should not cut through a blade (and if it has to it should do it perpendicular to the surface and not in a critical flow region), it should avoid the wake of the blade, and if possible it should avoid any shocks/rarefaction waves (but this can be very difficult to do, just minimise it as best you can).
But if you have a good mesh quality and a well converged solution you can get away with some of these sins. |
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June 3, 2012, 07:43 |
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#3 |
New Member
Alessio
Join Date: May 2012
Posts: 9
Rep Power: 14 |
Thanks for the help
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