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September 14, 2012, 13:15 |
Transonic Fan Optmization
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#1 |
Senior Member
Saima
Join Date: Apr 2009
Location: Canada
Posts: 185
Rep Power: 15 |
Hello Guys,
I have a quick query: Regarding Transonic Compressor Fan optimization. I am doing Aerodynamic optimization for compressor fan but have a problem to set back pressure. When Fan shape is changed during optimization the back pressure no more good for new blade shape. As one of the constraint for optimization loo is to have 0.5% diff of mass flow rate. But because P2/back pressure no more good so it is not able to get mass flow rate tolerance. Do you have any clue or idea to set that. Regards,
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Best Redards, Saima |
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December 25, 2012, 09:08 |
i have the same problem
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#2 |
New Member
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i need the geometry if u can help me ,, how u can get the geometry ?? are u using vista AFD
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December 25, 2012, 11:55 |
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#3 |
Senior Member
Saima
Join Date: Apr 2009
Location: Canada
Posts: 185
Rep Power: 15 |
For geometry creation we have our in-house software.
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Best Redards, Saima |
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December 26, 2012, 03:56 |
what do mean by house software??
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#4 |
New Member
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what do mean by house software?? i need a parametric geometry that can be used in ansys globe optimization>>>thanks for reply
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