✅ ANSYS CFX - NACA 4412 - Structured Mesh - Part 4/4

[@ansys_cfd]

Here all tutorials about this:
SPACECLAIM
ruclips.net/video/xkEvS5eafCg/видео.html
ruclips.net/video/bZN6rTcddQM/видео.html
DESIGN MODELER
ruclips.net/video/jRygry-RF6g/видео.html
ruclips.net/video/NVdHsqdMKGE/видео.html
ANSYS MESHING
ruclips.net/video/FPWQu1oL7V8/видео.html
ANSYS CFX
ruclips.net/video/_Uz3x18MXAo/видео.html
Regards

[@firmanzhahrial3161]

your video really helpfull, thank you so much and keep the great work!

[@ansys_cfd]

Hi friend; Thank you very much!
We going to do three giveaway, if you want to participate please review this link.
cfd.ninja/5th-anniversary/
Best Regards

[@soto6942]

I really love your videos, you are the best.
Do you have a bingham plastic tutorial on CFX?

[@ansys_cfd]

Thank you friend;
Sorry for the moment I dont have tutorials about that topic.
Regards

[@AdilKhan-gc8zu]

it is asking for parameters but in video its not showing, what i do now?

[@mahmoudabdelsalam100]

hi , i was working on axial compressor blade and i face a big problem to valid the cfd results with the experiment results , can u help me ?

[@ferielbou9398]

hi , can you please help me in NACA 4415 airefoil 3D meshing ???? i saw many tutorials but it's not realy clear close to the leading edge???thnks

[@KarthiKeyan-pd1xb]

If i want to validate the airfoil experimental results with simulation, what parameter should i select pressure coefficient or lift??? how to vary the meshing elements?>

[@ansys_cfd]

Hi my friend, if you want to validate you need the velocity of the experiment, and simulate with his NACA. Lift and Drag are calculated automatically. Regards

[@KarthiKeyan-pd1xb]

for validation purpose, what should be consider, first we attain lift and drag forces compared to experimental or CP?

[@ansys_cfd]

Hi my friend I think that Lift and Drag. Regards

[@shemafonso3206]

After doing this tutorial i was running another airfoil but When i try to run solutions I'm getting 'update failed for solution component in fluid flow. The solver failed with non zero exit code of 2'. Pls help...

[@ansys_cfd]

Hi friend; They can be several things, please check your mesh and your geometry, they must be clean (without errors), check the steps of the tutorial, you may have omitted any, also check the dimensions of your geometry. Regards

[@shemafonso3206]

@@ansys_cfd . Thnx , actually i solved it. I had created too many mesh nodes. I reduced them

[@ansys_cfd]

Great friend!
Best regards

[@KarthiKeyan-pd1xb]

Is it possible to attain Y+ less than 1 and aspect ratio less than 200...;..

[@ansys_cfd]

+Karthi Keyan hi my friend yes os possible but your mesh must be smaller and for this reason is posible that you need a good computational power

[@KarthiKeyan-pd1xb]

ok how can we bring aspect ratio below 200!!!!