|
[Sponsors] |
When will a shape optimization testcase terminate? |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
April 13, 2014, 13:02 |
When will a shape optimization testcase terminate?
|
#1 |
New Member
emily
Join Date: Mar 2014
Posts: 15
Rep Power: 12 |
According to the documentation Running SU2,"Objective functions (drag, lift, etc.) are determined running a direct flow solution in SU2_CFD and gradients are obtained using the adjoint solution. For each iteration in the design process, the mesh is deformed using SU2_MDC, and the analysis is repeated until a local optimum is reached."
I want to know that when will a local optimum be reached? What the exact meaning of it? It seems that it calls the SU2_CFD many times. When will the program terminate? |
|
April 13, 2014, 23:16 |
|
#2 |
Super Moderator
Thomas D. Economon
Join Date: Jan 2013
Location: Stanford, CA
Posts: 271
Rep Power: 14 |
Hi Emily,
SU2 uses the SLSQP algorithm that is available through the SciPy package in Python. You can find some more information about it here (including how to set the tolerance for the optimizer convergence): http://docs.scipy.org/doc/scipy-0.13...min_slsqp.html. Tom |
|
Tags |
shape optimization, terminate |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Airfoil Shape Optimization using gradient based methods | jaiswal | Main CFD Forum | 1 | April 10, 2014 12:22 |
Shape Optimization Error, Incorrect values produces by SU2_GDC | Dhig | SU2 Shape Design | 1 | March 20, 2014 06:58 |
Testcase for shape optimization using RANS simualtion | diwakaranant | SU2 Shape Design | 1 | April 18, 2013 14:27 |
Shape Optimization help | hannah72206 | ANSYS | 1 | June 25, 2012 18:15 |
CFD based robust hull shape optimization | Thouelfaqar | Main CFD Forum | 0 | October 13, 2011 15:44 |