Learning Forum

[AlfredOloo]

Hi,

I want to plot a graph of Coefficient of Drag for a 3D airfoil at various Angles of Attack.

I have done a simulation in ANSYS FLUENT with the Angle of Attack as the INPUT PARAMETER and the Drag force as the OUTPUT PARAMETER. 

I should be using the formula shown below within the PARAMETER SET....

 

MY QUESTION is this, what should I include as my reference area (S)? And how do you calculate it for various AoA?

 

Thank you.

[Amine Ben Hadj Ali]

Good article: https://www.grc.nasa.gov/WWW/K-12/airplane/sized.html#:~:text=Like%20the%20other%20aerodynamic%20force,used%20in%20the%20drag%20equation.

[AlfredOloo]

Thanks Amine for the link.

I understand the concept of the reference area from the link you shared. In this case, I am taking the projected area of the aerofoil looking at it directly from the leading edge.

Now, how do we calculate that (the projected area)? Can ANSYS automatically calculate it for various angles of attack? 

Since the lift and drag forces can be Automatically generated within ANSYS, can the same be possible with their coefficients?

 

Thank you

[Amine Ben Hadj Ali]

Yes it can: under Report-> Projected Areas

[AlfredOloo]

Then how do we calculate the coefficients of lift and drag using this this area for various AoA

[Amine Ben Hadj Ali]

By changing the reference area or you do it in third party or via UDF: if you have the force and you now the direction vector you want to look you can do everything outside of Fluent.

[AlfredOloo]

Actually, I got the solution to my question: When creating the lift and drag coefficients, there is an option for setting them as output parameters. This would solve my problem. With the Cl and Cd set as output parameters, I can then auto-calculate them by only changing the AoA and the inlet velocity.

 

Regards.

[Amine Ben Hadj Ali]

Perfect!

[Nabeel]

I am in need of a similar solution, can you please explain this in a bit more detail ?

[vishwajit patil]

Hello

I am also doing a similar experiment where i want to find the coefficient of drag and rolling momnet for a rocket at various fin cant angle. For creating a 3D model,  I integrated 8 geometries of the parts if rocket. I created the enclosure and there was no problem but when I started meshing, then the software didnt create the mesh and said there were a lot of problems. I am stuck now and i have to submit this by monday. What should i do?

 

[Rob]

Start a new thread for attention, but I also advise reviewing the training on Learning to see why you're getting the errors. Note, staff don't work weekends and given timezones responses aren't always within 24 hours. 

[vishwajit patil]

Here is the file and all the errors that are present.

[Rob]

Please read my previous comment.