|
[Sponsors] |
Continuous adjoint converge issue in transonic airfoil shape design |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
December 15, 2019, 10:13 |
Continuous adjoint converge issue in transonic airfoil shape design
|
#1 |
New Member
Join Date: Nov 2018
Location: Poland
Posts: 7
Rep Power: 8 |
Hello everyone !
I am dealing with shape design problem and I have got some questions about adjoint parameters, thus I have troubles with converge adjoint calculations. My direct case was converged well.
To the flow solution I use RANS solver with SA turbulence model, Mach number is 0.85 and Re= 4.6e6. Direct calculation converged well with CLF number = 50, FGMRES linear solver with LU_SGS preconditioner, entropy fix coefficient = 0.5, second order flow equation and first order turbulence equation. I attach config file, mesh, screenshots, solutions and restart solution files in link below. I got stuck on this problem for several weeks and would appreciate if someone could help me. https://github.com/zloty001/CRM_ShapeDesign Regards, zloty Last edited by zloty001; December 23, 2019 at 05:38. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Discrete vs Continuous Adjoint solution variable: Scaling/normalization issue? | asitav | SU2 | 2 | November 21, 2018 20:11 |
High drag for airfoil compared to XFOIL and wind tunnel data | Ry10 | SU2 | 15 | October 30, 2016 18:27 |
Fluent Adjoint Solver Convergence Issue? | ex10148 | FLUENT | 2 | July 25, 2016 15:41 |
[DesignModeler] Airfoil generation issue | micro11sl | ANSYS Meshing & Geometry | 1 | March 15, 2012 17:09 |
Question about Continuous Adjoint Method | fumiya | Main CFD Forum | 6 | November 1, 2011 11:09 |