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mecbe2002 February 21, 2012 03:24

Multi-Stage turbine analysis
 
Hi all,

I want to simulate a 5-stage gas turbine. The geomerty details are a follows,
  • Stage-1 -> Stator - 4 blades, Rotor - 9 blades
  • Stage-2to5 -> Stator -7 blades, Rotor - 9 blades
To start with i am planning to use "Mixing Plane Model". I need some help in how to mesh the geometry (particulary defining the interfaces) and is it possible to use periodicity?

Thanks
KGN


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