Fluids

Fluids

VAWT – 1dof system producing average torque = 0 and TSR = 0.06

    • toftegaard23
      Subscriber

      I am simulating a H-rotor VAWT (Vertical Axis Wind Turbine) with three blades using ANSYS Fluent, and I have set up the rotor to allow free rotation around its centre axis (1dof system). My inlet wind speed is 15 m/s, I’ve made ANSYS calculate the moment for each timestep and I use NACA0018 as the aerofoil-design type. After approximately 5 seconds (transient study with the blades standing still to begin with), the rotor has reached a steady state, and from the motion history written, I can see the angular velocity corresponds to a tip speed ratio of 0.06. Furthermore, the average of my moment values is very close to zero, which makes sense in that the rotor is not accelerating – it rotates with a constant speed. However, power is calculated as the product of the average torque and angular velocity, but since the average torque is zero, then I don’t produce any power, which shouldn’t be the case?


       


      I have also tried to set the rotor to rotate with a constant angular velocity that corresponds to a TSR = 4. This gives me torque-values that are negative for a positive angular velocity, hence the power is negative. This means the rotor needs to receive energy to maintain its rotational velocity, which again is contradictory to how a wind turbine works.


       


      One thing, I am not sure about is how you can include the resistance by the generator, since this depends on the magnetic flux etc.? One of my professors said that because I do not include frictional resistance in the simulation, then the simulation can either go to infinity, since there is nothing slowing it down, or it can reach a steady state, which is what has happened to mine. I just don’t understand why I got the second option? And why I get the solutions and numbers that I get?


       


      Appreciate your time and any input can be a massive help.

Viewing 0 reply threads
  • You must be logged in to reply to this topic.