Menu

Discussion Forum

New Discussion
Filtrer

Discussion Closed This discussion was created more than 6 months ago and has been closed. To start a new discussion with a link back to this one, click here.

Compute the moment on an wing

Posted 1 août 2017, 16:33 UTC−4 0 Replies

Cedric Pepin
Send Private Message Flag post as spam

Please login with a confirmed email address before reporting spam

Hi,

I have done a 2D CFD of a wing in a air flow. With this I can compute the drag and the lift with those expressions spf.T_stressx ; spf.T_stressy. But I don't know how to compute de moment about an axis. Does anybody know what is the expression?

Thank you
0 Replies Last Post 1 août 2017, 16:33 UTC−4
COMSOL Moderator

Hello Cedric Pepin

Your Discussion has gone 30 days without a reply. If you still need help with COMSOL and have an on-subscription license, please visit our Support Center for help.

If you do not hold an on-subscription license, you may find an answer in another Discussion or in the Knowledge Base.

Note that while COMSOL employees may participate in the discussion forum, COMSOL® software users who are on-subscription should submit their questions via the Support Center for a more comprehensive response from the Technical Support team.

Suggested Content