Ironcold
Guest
Hello everyone,
I will try to be brief,
after analyzing the aerodynamic behaviour of a naca0018 wing profile for wind turbines, at very low reynolds numbers, with mesh made in icem and fluent analysis, as next step I would like to understand how to set the oscillation problem of this profile...in practice I have the profile that oscillates with a speed of about 500 rpm between -10 and 10 degrees.
I would like to know from someone who knows more about me how to set up the problem, at university they told me how to wander, to use a fluent's sdof udf but they are at first arms and need help.
I did a search on the net, but I didn't find anything constructive.
Thank you in advance
savior
I will try to be brief,
after analyzing the aerodynamic behaviour of a naca0018 wing profile for wind turbines, at very low reynolds numbers, with mesh made in icem and fluent analysis, as next step I would like to understand how to set the oscillation problem of this profile...in practice I have the profile that oscillates with a speed of about 500 rpm between -10 and 10 degrees.
I would like to know from someone who knows more about me how to set up the problem, at university they told me how to wander, to use a fluent's sdof udf but they are at first arms and need help.
I did a search on the net, but I didn't find anything constructive.
Thank you in advance
savior