|
[Sponsors] |
How to calculate the AoA (Euler angles) in 6DOF model? |
![]() |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
![]() |
![]() |
#1 |
New Member
Cheng Jie
Join Date: Nov 2011
Posts: 8
Rep Power: 13 ![]() |
Hi Foamers,
Now I am simulating a case with sixDoF dynamic mesh model (similar to FOAM_TUTORIALS/incompressible/pimpleDyMFoam/wingMotion/wingMotion2D_pimpleDyMFoam). During the post-process, all I want is the curves between Angle of Attack and lift coefficient. But I have no idea about how to calculate the AoA in this kind of aero-actuated model. Does any one have any experiences? ![]() Jie |
|
![]() |
![]() |
![]() |
Tags |
aoa, post-processing, sixdof |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Euler Granular Model | Sashankh | FLUENT | 1 | January 29, 2017 12:41 |
manualInjection model in sprayFoam | Mentalo | OpenFOAM Running, Solving & CFD | 1 | April 2, 2014 09:29 |
K - epsilon VS SST turbulence model | Maicol | Main CFD Forum | 0 | November 30, 2012 16:25 |
Does CFX can calculate within structure model? | prayskyer | CFX | 9 | November 28, 2006 23:13 |
Euler Model | bharath | Main CFD Forum | 0 | November 13, 2002 12:31 |