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.

3D k-epsilon for flow over cylinder with Re~700. C_d is too low. Any suggestions???

Please login with a confirmed email address before reporting spam

Hi!

I have used the k-epsilon turbulence model with stationary solver to simulate airflow over a circular cylinder with radius 1 mm, and inlet flow of U =5m/s.

This should yield a drag coefficient of around 1, but my output shows 8.15. I've used the guidance of the "how to compute lift and drag" blog, to calculate the drag coefficient. Is the inaccuracy in the mesh( I used extra fine), or in the k-epsilon model? Since there will be adverse pressure gradients, should I use k-omega instead? Or is it the turbulent length scale? (I didn't use 0.07*diameter...)

I've attached the model without results since it was too large.

I'm forever grateful for any responses!

0 Replies Last Post 10.08.2017, 07:33 GMT-4
COMSOL Moderator

Hello Brynjulv Tveit

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.