|
[Sponsors] |
SU2 shape optimization initialization method? |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
April 10, 2015, 05:49 |
SU2 shape optimization initialization method?
|
#1 |
New Member
Zhang Rui
Join Date: Oct 2014
Posts: 15
Rep Power: 12 |
Dear friends in SU2,
I am concerned about the initialization of fluid field in every iteration.Does Su2 use the same 0 as the initialization quantity to initialize the physical field in every iteration after the mesh change? I think it is quite a time-consuming method. Can SU2 use the convergent solution of previous step to initialize the field and use the dynamic grid as well? Waiting for someone to help me. Yours, Gina |
|
May 2, 2015, 17:40 |
|
#2 |
New Member
Daquan He
Join Date: Aug 2014
Posts: 7
Rep Power: 12 |
Yes, SU2 uses the nearest design's results as the initial starting state for the next flow evaluation. The state's attribute 'state.pullnlink' gets the file names of nearest design's results, and the 'redirect' function is used to link the results files to the new design folders. Hope this will help you. A further look into the code, or carry out step by step operation according to the python code manually, then you will find that.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
CFD based robust hull shape optimization | Thouelfaqar | Main CFD Forum | 0 | October 13, 2011 15:44 |
Shape optimization | DoHander | Main CFD Forum | 0 | April 28, 2011 23:28 |
Shape Optimization | francesco_capuano | FLUENT | 2 | April 28, 2011 12:51 |
Shape optimization | chuls | Main CFD Forum | 1 | October 6, 2009 05:00 |
SQP method for adjoint based aerodynamic shape optimization | cfdbooks | Main CFD Forum | 2 | May 26, 2009 11:40 |