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March 5, 2018, 14:44 |
Aerodynamic coefficients
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#1 |
New Member
Andrea Visentini
Join Date: Feb 2018
Posts: 1
Rep Power: 0 |
Hi everybody,
this is my fist post in this forum, I have a problem with Numeca software. I have an aerodynamic profile in a simple domain, I have make the mesh ad start the solution with Fine Open. In the monitor compre the Lift and Drag force, my question is: can I see directly the value of the aerodynamic coefficients Cl and Cd? If so where? Tnk Andrea |
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March 6, 2018, 16:16 |
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#2 |
Senior Member
Holger Dietrich
Join Date: Apr 2011
Location: Germany
Posts: 174
Rep Power: 15 |
Dear Andrea,
yes, it is given out by one of the standard files of the computation. Please have a look into the computation directory, at the bottom of the .wall file the computed lift and drag coefficient with its reference values is given out. You can easily access this file with any text editor. Please make sure that you have set in the FINE/Open GUI -> Computation Control -> Outputs to "External Flow". Kind regards Holger |
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November 4, 2019, 02:30 |
cl and cd
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#3 |
New Member
veerappan
Join Date: Apr 2019
Posts: 15
Rep Power: 7 |
after my computaion , i cant see cl and cd values ..its showing zero values , its not updating
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November 13, 2019, 05:25 |
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#4 |
Senior Member
Colinda
Join Date: May 2012
Location: Brussels
Posts: 153
Rep Power: 14 |
Did you activate the "compute force and torque" for the applicable solid patches in the solid boundary conditions page?
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February 24, 2020, 05:30 |
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#5 |
New Member
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Last edited by massimiliano.tarrini; March 3, 2020 at 03:58. |
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