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Automatic Simulation of 2D Airfoil Section at Different Angles of Attack |
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#1 |
Senior Member
Ali
Join Date: Jan 2012
Location: Pakistan
Posts: 134
Rep Power: 17 ![]() |
I want to perform the CFD simulation of 2D airfoil such that:
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#2 |
Senior Member
Ali
Join Date: Jan 2012
Location: Pakistan
Posts: 134
Rep Power: 17 ![]() |
Any suggestion, help!!!
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#3 |
New Member
Join Date: May 2012
Posts: 3
Rep Power: 14 ![]() |
I have a script that
imports stp file (containing airfoil made in CATIA) meshes around it using ICEM computing the solution in FLUENT If you have this knowledge I see no reason you couldn't edit the CATIA model to an aoa then import and analyse. It is a bit of a task to get it all automated but it is possible. |
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#4 |
Senior Member
Ali
Join Date: Jan 2012
Location: Pakistan
Posts: 134
Rep Power: 17 ![]() |
Will you share your script? I will PM my email to you.
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Tags |
automation, fluent, udf, workbench |
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Thread | Thread Starter | Forum | Replies | Last Post |
2D SST Simulation Airfoil - Convergence Problem | Kraemer | CFX | 10 | April 16, 2011 07:22 |
Flows at High Angles of Attack | Sarah C. | FLUENT | 2 | March 18, 2009 07:39 |
NO STAGNATION POINT FOR AIRFOIL SIMULATION | Rif | Main CFD Forum | 6 | February 4, 2008 07:33 |
Airfoil Simulation for Validation Purposes | Angela Bong | Main CFD Forum | 7 | September 13, 2006 13:04 |
iteration on angles of attack | Vincent | FLUENT | 4 | May 13, 2005 11:31 |