How to Calculate Lift and Drag of NACA 2412 Airfoil Wing in ANSYS | ANSYS Fluent Tutorial | Part 2

Buy PC parts and build a PC using Amazon affiliate links below -

In this tutorial, we will learn how to do geometry preparation for a wing cad model and calculate lift and drag on the wing. In this video part 2, the procedure of geometry preparation, meshing, setting up boundary conditions, and calculating lift and drag results has been demonstrated.

[jamesrand]

A really useful video series going through the whole process of using ansys - well done CFD Baba

[yacob]

Really helpful, I hope you upload more videos like this, and please do it frequently!!

[harshvardhansharma]

you much brother you saved me from failing semester project your method helped me a thank u so much

[sam]

Thanks CFD BABA, Videos are clear for learning how to use the software.

[christosvasiliou]

so you dont have to do this on the solution tab where you create a graph for whatever you want, you just calculate the problem and you can do this on the result-post processing part ? the number it shows you for the force, is calculated for 200 interations as well ?

[cfdbabaopenfoamansyscfd]

Hello CFD Analysts. Thanks for all the response and support. However, 92.16% of viewers have not yet subscribed to this channel. Please consider subscribing for more such new CFD videos. Also, don't forget to comment on your favorite part of the video below and suggest topics on which you want videos in the future.

[joelquiralte]

This video save my Lab Report, very useful and well explained

[engineered.mechanized]

How do I analyze the resonant frequencies experienced by a steel cylinder under water flow?

[knjjcbs]

How you saved the file as stp? I cant find that format. Is it okay to continue working on the existing drawing from part 1 and continue the the part video without importing it again as stp file?

[nurshuhadanajwabintimohdsh]

hi just wanna ask if the wing have winglet how to select the inner side? its hard for me to select

[mukutvlog]

Thanks for the nice in-depth tutorial. subscribed.

[jameszulu]

Thanks for your help. This video was really helpful.... Baraka Allahu fik😉

[fayssalcheriet]

A very helpful tutorial thank you, can do one for FSI tutorial.

[Deadshotuno]

thank u so much this was very helpful for my school assignment

[neetur-idfi]

Excellent explanation & very informative... keep it up.

[prathameshsahoo]

How to apply dynamic meshing using udf to similar simulations
I have to simulate an oscillating 3d wing
Can you help please?

[cebeciemir]

one or more entities failed to mesh error what can i do for it

[sujitroy]

The lift and drag force calculated in the video is for half wing or for the full wing, as symmetry is used. If one wants to calculate lift and drag coefficient from the generated lift and drag force, what will be the span length (3 m or 1.5 m).

[hemanthlucky]

sir how can we find forces at different angle of attacks. please reply 🙏

[brudhelbamokila]

Hello,

Thanks for this video. I am studying the flow around a 3D wing and would like help with the reference values ​​to be specified in Ansys Fluent. I know the area is the top surface of the wing, the length is that of the chord. But my problem is that the chord is not constant all the way down the wing (the chord at the root is bigger than the salmon one). How can I specify the chord in this case, please ?