Forum: Main CFD Forum
March 16, 2012, 02:56
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Replies: 51
Views: 20,848
Hi Hemant,
I have tried different turbulence...
Hi Hemant,
I have tried different turbulence models without much success: It sems that only LES should give something more or less close to reality.
I have also tried the following thing with...
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Forum: Main CFD Forum
March 17, 2011, 15:28
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 15, 2011, 16:52
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 14, 2011, 16:05
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 14, 2011, 15:37
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Replies: 51
Views: 20,848
I am still confused: At figure 4 of that...
I am still confused: At figure 4 of that reference they list k-w sst, k-w sst trans., gamma-re-theta. So it sems that they distinguish between k-w sst trans and gamma-re-theta. At that figure k-w...
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Forum: Main CFD Forum
March 14, 2011, 07:58
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Replies: 51
Views: 20,848
There is quite a confusion with the names of...
There is quite a confusion with the names of models in Ansys/Fluent.
I found another reference that has comparison different models with gamma re theta and sst-for transitional flows among them...
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Forum: Main CFD Forum
March 13, 2011, 03:05
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Replies: 51
Views: 20,848
Joshua,
The published papers you gave (I do...
Joshua,
The published papers you gave (I do not have access to one by Alam) seem to discuss flows at re of several millions (perhaps your coming paper will present results on smaller re).
Do...
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Forum: Main CFD Forum
March 11, 2011, 18:22
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Replies: 51
Views: 20,848
Thanks for Info: Did you do steady or unstedy...
Thanks for Info: Did you do steady or unstedy simulations, if unsteady/transient what was the timestep? What was the resolution of grid (in direction of normal and along airfoil surface) and boundary...
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Forum: Main CFD Forum
March 11, 2011, 01:50
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Replies: 51
Views: 20,848
I have access to fluent 6.3.26 and it has s-a,...
I have access to fluent 6.3.26 and it has s-a, k-e, k-w, k-w sst, k-w sst transitional, and Reynolds Stress: I could not get decent results with k-w sst transitional for sd7037 at RE=70000.
I know...
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Forum: Main CFD Forum
March 9, 2011, 16:40
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Replies: 51
Views: 20,848
Thanks a lot Martin,
For SA I got cd around...
Thanks a lot Martin,
For SA I got cd around 2.7E-2 and Cl around .75, but for k-w standard Cd is about 7E-2, which is completely unacceptable.
I was directed to interesting articles that...
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Forum: Main CFD Forum
March 9, 2011, 03:04
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 9, 2011, 01:45
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Replies: 51
Views: 20,848
here is the close up for kw-sst for trailing...
here is the close up for kw-sst for trailing edge. Also residuals for
kw-steady -> kw-unsteady -> kwsst-unsteady
Time step: (1% of airfoil chord flow travel per time step, max 10 iterations per...
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Forum: Main CFD Forum
March 9, 2011, 01:35
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 8, 2011, 17:39
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Replies: 51
Views: 20,848
The problem here that there is no experimental...
The problem here that there is no experimental results for stepped vortex-trapping airfoils, analysys of which is a final goal of thisn work. I wanted to compare performance of this type of airfoils...
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Forum: Main CFD Forum
March 8, 2011, 17:27
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 8, 2011, 17:12
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Replies: 51
Views: 20,848
Thanks Martin,
Seems you are right, see...
Thanks Martin,
Seems you are right, see plots for steady simulation form kw (2000 iterations) to kw sst staedy with oscillating residuals (they are also shown). The eddy viscosity is too small....
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Forum: Main CFD Forum
March 8, 2011, 16:15
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 8, 2011, 15:57
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 8, 2011, 03:21
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Replies: 51
Views: 20,848
No, I mean numeric convergence, i.e. reasonable...
No, I mean numeric convergence, i.e. reasonable decrease in resudual. I have tried both stationar and non-stationar solvers: residuals oscillate wildly in kw-sst transitional model. Perhaps indeed...
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Forum: Main CFD Forum
March 8, 2011, 03:08
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Replies: 51
Views: 20,848
Thank you for suggestion, swithching
...
Thank you for suggestion, swithching
k-omgega ---> k-omega sst ----> k-omega sst transitional
does not help: k-omega goes fine, then k-omega sst still have acceptable residuals, but when...
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Forum: Main CFD Forum
March 7, 2011, 11:48
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Replies: 51
Views: 20,848
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Forum: Main CFD Forum
March 7, 2011, 05:03
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Replies: 51
Views: 20,848
Two-equation turbulent models: low re airfoils
Hello
I am trying to analyse flows past different 2D airfoils at low reynolds numbers (order of 10^4-10^5) and having problems. I am using fluent, but I guess this is not the fluent problem, but...
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