CFD Parametric solution

    • bilal ojaily


      I am studing on wing to calculate CL and CD in different angle of attack, and I heard there is a method (parametric solution) like a loop to calculate it by changing angle of wing or velocity vector

      how can I use this method?

    • Rob
      Ansys Employee

      By setting a parameter to alter the geometry (less efficient) or inlet velocity components (more efficient). However, read through the NACA examples in Help (tutorial and/or video) as force and coefficient reporting is a little less trivial. 

Viewing 1 reply thread
  • You must be logged in to reply to this topic.