hexagon logo
Register Sign in
  • State Not Answered
  • Replies 9 replies
  • Subscribers 8 subscribers
  • Views 112 views
  • Users 0 members are here
Options
Related

Hello guys, I am trying to study the flow around NACA0012 airfoil at zero angle of attack. However, when I try to refine the octree parameter around the airfoil and generate the mesh, every single time I get different values for Lift force! Any reasons??

hossam
Hello guys, I am trying to study the flow around NACA0012 airfoil at zero angle of attack. However, when I try to refine the octree parameter around the airfoil and generate the mesh, every single time I get different values for Lift force! Any reasons??
Parents
  • 0
    Hello Chuel,
     
    It worked! I put wrong BCs. on top and bottom of the domain.
    Is there a way to get the value of the drag only? I need to understand why the value here in X is by negative. The lift value is fine for me, however the value in X is suspicious for me. Does it relate to the kind of surface forces I need to compute during the setup?
    Capture2
Reply
  • 0
    Hello Chuel,
     
    It worked! I put wrong BCs. on top and bottom of the domain.
    Is there a way to get the value of the drag only? I need to understand why the value here in X is by negative. The lift value is fine for me, however the value in X is suspicious for me. Does it relate to the kind of surface forces I need to compute during the setup?
    Capture2
Children
No Data
© 2025 Hexagon AB and/or its subsidiaries. Privacy Policy | Cloud Services Agreement