Forum: OpenFOAM Running, Solving & CFD
July 7, 2014, 06:20
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Replies: 30
Views: 4,574
Need a paper
Hi,
Anybody is having this paper ?
O. Borm et al., Density based navier stokes solver for transonic
ows," OpenFoam 6th workshop, 2011.
I am in need this the paper . Please share with me .
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Forum: OpenFOAM Running, Solving & CFD
June 26, 2014, 02:47
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Replies: 30
Views: 4,574
Turbo Performance Problem
Hi,
I have improved the quality of mesh and checked the mesh quality before simulation. It gave Mesh OK message. Now simulation is going on.
But i have attached turbo performance code in...
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Forum: OpenFOAM Running, Solving & CFD
June 24, 2014, 04:22
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Replies: 30
Views: 4,574
Output of the command
...
Output of the command
sml5kor@BMH301562:~/OpenFOAM/sml5kor-1.6-ext/run/TURBINE_cyclicGGI_2/finel_merge_2/Case_with_initial_volcity_field_high_k-omega$ checkMesh -allTopology -allGeometry...
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Forum: OpenFOAM Running, Solving & CFD
June 24, 2014, 03:12
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Replies: 30
Views: 4,574
transonicMRFDyMFoam
HI Dowlee,
I have set up the case of radial inflow turbine passage and case is running absolutely fine.
But after convergence whyc there is a difference in mass flows at the inlet and outlet....
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Forum: OpenFOAM Running, Solving & CFD
May 28, 2014, 06:56
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Replies: 30
Views: 4,574
No convergence with transonicMRFDyMFOAM
Hi,
I have simulated the case. Up to 1400 iterations everything went well. Ang got the results almost converged. Which is as follows
Time = 1400
MassFlows: INLET = 0.050998309
MassFlows: ...
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Forum: OpenFOAM Running, Solving & CFD
May 27, 2014, 04:52
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Replies: 30
Views: 4,574
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Forum: OpenFOAM Running, Solving & CFD
May 23, 2014, 04:19
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Replies: 30
Views: 4,574
No convergence
Hi,
I have changed some BC in velocity. As i knew flow rate for my case I gave as follows
INLET
{
type flowRateInletVelocity;
flowRate ...
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Forum: OpenFOAM Running, Solving & CFD
May 22, 2014, 04:42
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Replies: 30
Views: 4,574
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Forum: OpenFOAM Running, Solving & CFD
May 21, 2014, 07:36
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Replies: 30
Views: 4,574
mass flow problem
Hi,
Now the case is running but gives some error after some 100's of iterations.
The error is as follows
Time = 2000
diagonal: Solving for rho, Initial residual = 0, Final residual =...
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Forum: OpenFOAM Running, Solving & CFD
May 19, 2014, 09:57
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Replies: 30
Views: 4,574
mass flow Out of range
Hi ,
I tried with inletOutlet BC at OUTLET patch and laminar case but the output of mass flow remains the same .. which is as shown below. ...
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Forum: OpenFOAM Running, Solving & CFD
May 19, 2014, 06:49
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Replies: 30
Views: 4,574
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Forum: OpenFOAM Running, Solving & CFD
May 19, 2014, 05:35
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Replies: 30
Views: 4,574
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Forum: OpenFOAM Running, Solving & CFD
May 19, 2014, 05:28
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Replies: 30
Views: 4,574
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Forum: OpenFOAM Running, Solving & CFD
May 19, 2014, 04:25
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Replies: 30
Views: 4,574
"libsimpleFunctionObjects.so"
functions
(
inletMassFlow
{
type patchMassFlow;
functionObjectLibs
(
"libsimpleFunctionObjects.so"
);
verbose true;
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Forum: OpenFOAM Running, Solving & CFD
May 19, 2014, 01:28
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Replies: 30
Views: 4,574
BC and Constant files
Hi,
Please find the attached BC and Initial values of the case which has run but wrong mass flow. Let me know your feed back upon this .
Regards,
Sam
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Forum: OpenFOAM Running, Solving & CFD
May 17, 2014, 05:14
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Replies: 30
Views: 4,574
I was able to run the case but after 1000...
I was able to run the case but after 1000 iterations I am getting wrong flow rate .
Time = 1000
diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal:...
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Forum: OpenFOAM Running, Solving & CFD
May 15, 2014, 02:01
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Replies: 30
Views: 4,574
Hi,
1. Can you provide me the typical...
Hi,
1. Can you provide me the typical boundary condition provided by Borm. ? Means where I can find them.
3. frozen rotor. means MRF method as Borm used in transonicMRFDyMFoam solver .
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Forum: OpenFOAM Running, Solving & CFD
May 12, 2014, 23:53
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Replies: 30
Views: 4,574
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Forum: OpenFOAM Running, Solving & CFD
April 29, 2014, 01:46
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Replies: 30
Views: 4,574
Hi
Hi Trent,
Have you been able to run transonicMRFDyMFoam case of your's successfully ?
I need some help in this regard.
Can you please help me ?
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