|April 29, 2014, 06:30||
boundary conditions to minimize drag
Join Date: Apr 2014
Posts: 19Rep Power: 4
I'm trying to use AdjointShapeOptimizationFoam to optimize a drag coefficient of an airfoil.
I need to define boundary conditions wrt. cost function of drag coefficient. I have already seen in literature (Othmer) how to define the boundary conditions to minimize total pressure loss or power loss for ducted flows, but unfortunately I don't understand how should I change "adjointOutletPressure" and "adjointOutletVelocity" to minimize the drag coefficient of an airfoil?
So far, I've set Ua and pa = 0 at the inlet and at the outlet, because only the airfoil contour is important for this problem, but I still don't get how should I adjust the adjoint boundariy conditions at the airfoil contour?
I hope someone can help me at this
|May 26, 2014, 09:21||
Join Date: Mar 2009
Posts: 64Rep Power: 9
This paper was helpful to me (On the Computation of Flow Sensitivities from Boundary Integrals):
|boundaries, drag, minimize|
|Thread||Thread Starter||Forum||Replies||Last Post|
|Question about heat transfer coefficient setting for CFX||Anna Tian||CFX||1||June 16, 2013 06:28|
|Low Mixing time Problem||Mavier||CFX||5||April 29, 2013 00:00|
|boundary conditions and mesh exporting||vaina74||Open Source Meshers: Gmsh, Netgen, CGNS, ...||2||May 27, 2010 09:38|
|Trimmed cell and embedded refinement mesh conversion issues||michele||OpenFOAM Other Meshers: ICEM, Star, Ansys, Pointwise, GridPro, Ansa, ...||2||July 15, 2005 04:15|
|A problem about setting boundary conditions||lyang||Main CFD Forum||0||September 19, 1999 18:29|