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July 25, 2018, 21:01 |
Isolated Rotor Single Passage
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#1 |
New Member
Mohamed Abu-bakr Ibrahim
Join Date: Mar 2018
Posts: 11
Rep Power: 8 |
Currently, I am working on an unsteady analysis of a single passage of isolated rotor (no stator) of an axial compressor using cfx.
I can't decide which to use Transient or Transient blade row model. And if I should use transient blade row model, can I use time transformation in this case and if I can, how? Note my domain is 1 element including inlet blade passage and outlet, so there is no interface between them. The only interface exist are tip gap and periodic surface interface. Thank in advance. Last edited by Mohamed Abu-bakr; July 27, 2018 at 18:20. Reason: missing info |
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Tags |
axial blade, cfx, compressor, unsteady |
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