[Nek5000-users] Computing aerodynamic coefficients

[nek5000-users at lists.mcs.anl.gov]

Your code looks fine to me. If you have not used Nek5000 in a while, I would recommend to look at the turbChannel example that contains the logic to compute the drag.

Marco 
On 2/9/18, 6:49 AM, "Nek5000-users on behalf of nek5000-users at lists.mcs.anl.gov" <nek5000-users-bounces at lists.mcs.anl.gov on behalf of nek5000-users at lists.mcs.anl.gov> wrote:

    object