Forum: FLUENT
April 12, 2012, 13:09
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Replies: 27
Views: 5,139
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Forum: FLUENT
April 12, 2012, 09:44
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Replies: 27
Views: 5,139
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Forum: FLUENT
April 12, 2012, 00:24
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Replies: 27
Views: 5,139
I use a 20ms^-1 velocity inlet as told earlier,...
I use a 20ms^-1 velocity inlet as told earlier, and then use a pressure outlet with a 0 Pa guage pressure. At the ICEM CFD, I set the solver as fluent v6 and in the BC set the FFINLET and FFOUTLET...
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Forum: FLUENT
April 11, 2012, 00:56
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Replies: 27
Views: 5,139
Hello,
I'm using fluent 12.1, laminar model,...
Hello,
I'm using fluent 12.1, laminar model, AOA 0, velocity 25ms^-1, velocity inlet and pressure outlet. I got your reference values. While I used another mesh with aspect ration within 20 I had...
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Forum: FLUENT
April 10, 2012, 02:59
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Replies: 27
Views: 5,139
Mesh file
Hello people I have included the mesh file in the zip file attached, I still get the flow reversal problem :confused: And I have no clue about the reference are and lengths modification. The boundary...
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Forum: FLUENT
March 25, 2012, 03:07
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Replies: 27
Views: 5,139
helpful
I still haven't solved, but for anyone who has this same problem, you could use this information in the site
https://www.sharcnet.ca/Software/Fluent12/html/tg/node53.htm
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Forum: FLUENT
March 23, 2012, 09:54
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Replies: 27
Views: 5,139
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Forum: FLUENT
March 23, 2012, 05:43
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Replies: 27
Views: 5,139
Thanks on your reply
I have defined the walls are pressure fields and in the fluent I defined them as velocity inlet and pressure outlet, with a velocity of 20ms^-1, and the pressure outlet set to guage, 0Pa. I tried...
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Forum: FLUENT
March 20, 2012, 15:30
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Replies: 27
Views: 5,139
Airfoil 2D help
Hello ppl,
I'm trying to do a 2D airfoil analysis using ansys fluent, I used the 3 part tutorial video to mesh a CH type mesh in ICEM CFD, when I import into fluent the mesh imports fine,...
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