CFD Online Logo CFD Online URL
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Post-Processing

How to calculate the AoA (Euler angles) in 6DOF model?

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Search this Thread Display Modes
Old   August 27, 2014, 05:16
Default How to calculate the AoA (Euler angles) in 6DOF model?
New Member
Cheng Jie
Join Date: Nov 2011
Posts: 8
Rep Power: 14
jiec827 is on a distinguished road
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?

jiec827 is offline   Reply With Quote


aoa, post-processing, sixdof

Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On

Similar Threads
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

All times are GMT -4. The time now is 11:00.