Fluids

Fluids

CL_max in CFX

    • Sapir.Argavani
      Subscriber

      Hello,

      I'm trying to run an airplane at large angle of attack 

      I have a problem with my results, the wings are stalling at smaller CL and angle of attack then reality. 

      When I checked the imbalance I noticed that the rethetat is not equal to zero. I have checked the mesh already and now I am checking the size of my domain. 

      I would like to know if there is any method  of the solver (or other tips in general) which can help me solve this problem or if its.

      Thank you

    • Surya Deb
      Ansys Employee

      Hello, 

      Have you checked the flow field? Is there unexpected boundary layer separation happening?

      Also, did you try to perform a mesh refinement study , specially near the boundary layer of the airfoil?

      Regards,

      SD

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