 |
 |
 |
|
|
|
[Sponsors] | ||||
Cl history for pitching airfoil(i.e at changing AoA) |
 |
|
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
October 26, 2017, 11:52
|
Cl history for pitching airfoil(i.e at changing AoA)
|
#1 |
|
New Member
musab
Join Date: Oct 2017
Posts: 11
Rep Power: 8  |
Hello everyone...
I need your views/ideas. I am having serious problem and got stuck and dont know how to encounter that issue. The master's thesis submission date is around the corner. My question is about pitching airfoil In pitching airfoil case the angle of attack changes with time. In Solve/Monitors, we can plot CL history but that is for some 'fixed' angle of attack (as there is no option there to upload a UDF file). So, I want save CL values history at changing angle of attack. Can anybody tell me how to get CL history in this case? Really appreciate your views. Thanks in advance |
|
|
|
|
|
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| loading issue libraries:libsimpleFunctionObjects.so libsimpleSwakFunctionObjects.so | immortality | OpenFOAM Pre-Processing | 15 | April 7, 2024 12:35 |
| Changing AoA No effect | turbine_blade | Main CFD Forum | 0 | January 8, 2016 11:37 |
| [PyFoam] Problems with the new PyFoam release | zfaraday | OpenFOAM Community Contributions | 13 | December 9, 2014 18:58 |
| [PyFoam] having problems with pyfoam Installation | vitorspadetoventurin | OpenFOAM Community Contributions | 3 | December 2, 2014 07:18 |
| Wrong Drag and Lift Coefficient when changing AoA | inspiron | FLUENT | 1 | November 27, 2013 13:00 |
Linear Mode
