General Mechanical

General Mechanical

Determine lift and Drag at a particular altitude (10,000 ft)

    • AlfredOloo
      Subscriber

      Hi,


      I want to simulate the amount of LIFT and Drag in an AIRFOIL WING flying at an altitude of 10,000ft at a speed of 24m/s.


      Can someone show me what to change within ANSYS FLUENT to help me do this, please?


      At 10,000ft the pressure is about 69.7kPa.


       


      Thanks 

    • Rob
      Ansys Employee

      Have a look in the tutorials there's bound to be a NACA wing doing exactly this. 

    • AlfredOloo
      Subscriber

      Can I have the link to this please?


      Tried searching to no avail.


       


      Regards

    • Rob
      Ansys Employee

      Click on Help, and when you get to the online help there are tutorials. Alternatively search for Fluent aerofoil (might be airfoil) and you'll find some YouTube videos. 

    • AlfredOloo
      Subscriber

      Okay thank you

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