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Y+ Graph Airfoil Upper and Bottom Surface (NACA0006)

    • SilverRD
      Subscriber

      Hi! I need someone advice does my Y+ acceptable?

    • Murari Iyengar
      Ansys Employee
      The Yplus values lie in the log-law region ie. 30
    • SilverRD
      Subscriber
      I used Ideal gas, compressible free stream mach no. 0.8, AoA 4deg there's a visible shock on the upper surface of the airfoil. I'm not sure please correct if I'm wrong I think the shock on the upper surface cause the sudden drop? If it is, does my wall Y+ acceptable?

    • Rob
      Forum Moderator
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