Vertical Axis Wind Turbine (VAWT) simulation
I have done a steady state simulation of a vertical axis wind turbine. The solution has converged to a max residual of 1e-5 but i get an excessive torque value so I'm having my doubts on the physics setup.
The steps i have followed are: 1.- Draw the wind turbine blades 2.- Draw a cylinder around the blades (rotating fluid) 3.- Draw a large frustum around the blades 4.- Substract the cylinder from the frustum to obtain the outer volume shown in the image. 5.- Subtract the blades from the cylinder to obtain the inner volume shown in the image. https://i.imgsafe.org/c5bbf6b055.png * The cylinder containing the blades is set as a rotating domain with the design rotational speed of the turbine and Z rotation axis (turbine axis). * The frustum is a stationary domain. The boundary conditions i have used are: - Inlet the left and lateral faces of the frustum, with a velocity component in the X axis (free stream of air). - Outlet at the right face of the frustum. - Interfaces between the frustum and cylinder common faces, with frozen rotor frame change - Wall at the blades. My questions are: 1.- Is the physics setup correct? 2.- The real torque in the turbine oscillates with time due to the angular rotation and different angles of attack. The torque obtained by CFX is the average over time? 3.- What is the physical effect of increasing the volume of the cylinder around the blades (with rotating fluid) ? It currently contains the blades tightly (cylinder height = 1.2x blade height) |
Q1 - probably not. But you should do the first level of investigation yourself. Have a look in the post processor - do the streamlines look reasonable? Is the rotor rotating in the correct direction? Are you getting attached flow where you expect, and separations where you expect?
Q2 - If you modelled this as frozen rotor the torque returned is the instantaneous torque at this angle in the rotation. Q3 - It should be no effect. If this has an effect it shows there is a problem in your setup. |
jorge..how did you get an excessive torque value
i have followed same procedure which you have done.
i had make mesh in ICEM CFD 16.2 and run simulation in fluent 16.2 but i never got torque (moment) above 0. i have give the rotating zone to frame motion and my aerofoils are stationary wall. i have almost try all model like k-e (std and realizable), k-w(SST), S-A etc. please any one give me some idea. why this is happening with me.:confused: |
Try the fluent forum.
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hi ghorrocks;
thanks for your reply.but i dont know whats this fluent forum? |
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