|August 27, 2014, 05:16||
How to calculate the AoA (Euler angles) in 6DOF model?
Join Date: Nov 2011
Posts: 8Rep Power: 7
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?
|aoa, post-processing, sixdof|
|Thread||Thread Starter||Forum||Replies||Last Post|
|Euler Granular Model||Sashankh||FLUENT||1||January 29, 2017 13:41|
|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 17:25|
|Does CFX can calculate within structure model?||prayskyer||CFX||9||November 29, 2006 00:13|
|Euler Model||bharath||Main CFD Forum||0||November 13, 2002 13:31|