Can you do for 3d also 😢 same square model please

Hi I am doing 3d analysis for naca 0012 airfoil at various angle of attacks but even at higher angle of attacks the cl value is still increasing but visually the flow detached from the wing(Stall conditions). What can I do to solve this?

I click run and nothing happend

hi bro i was wondering what is your job, also from pakistan love your videos

Thank you very much

bro the tutorial was awesome but please look at the part where your screen froze at 37:00

hi bro this was nice tutorial but i cant select the faces which are inside the airfoil like you did in the video at 22:12 . please tell me solution for it

In plane section video paused

I need full project

How would you go about making an airfoil with tubercles, but with spanwise periodicity? As far as I can tell the only way is to make a tubercles airfoil with a larger span than desired and then chopping the ends of, but I was wondering if you knew a better way.

bro finally i find your video and i have downloaded you are the best love you bro from pakistan

What a nice tutorial! Thank you very much!

minute 40:00 froze

Hi thank you for this video! I'm following anything you said, anyway the extrusion of the body of influence messes up with the first extrusion and the boolean operation as well. All three operations show me an error, tried to suppress and redo as you show but its not working. If anyone knows where I might be wrong please reply

Sir permissible shear stress is 420mpa and we got in simulation 605 how the design is safe

What about the last portion of the video your screen are freezed

Sir could you please post simulation and motion study video of this and tubercles and it's my request.

If permissible shear stress is 420 mpa, and in simulation it is 605 mpa. Then how is our design safe?

hello Sir your video is not showing the process just after the Contour. Can you please Look into it

Sir actually my it 2024 there reference mate is only option to get planes what we should fo

bro when i created a second extrude ... it doesn't show as a different body, It stills shows a total of 1 body .... Rather than being two bodies SEE 15:15 and 15:21

Hey brother very good video I am getting error at Fluent setup i got error of " You are using student version can only be used with cases containing less than 1048570 cells. Please exit ansys fluent and start new " Please explain me what is cased and cells here and i how i overcome this error in airfoil analysis Please kindly recognize.

I need to create tubercles on leading edge of propeller. Can you help please?

Thank you

100% working

Torrents are banned

you are the best forever !! make another video plss

hello, ı cannot edit from setup. the programme gives an error is it because ı use the student version or what else ı cannot figure it out can you help me?

Brother jab hum torrent mobile main download karyn to kia VPN required hota hy

dont download file has virus can affect your privacy

Very funny assumptions that everything is fine. Moreover, he contradicts himself. The author shows the basic interface of Ansys and absolutely does not understand what he is doing, youtube is full of video like this...

Thanks for the video, how did you prepare the data before importing to the Geometry in 3d

Very helpful <3

Thank you keep up

Have been struggling for hours but your method worked very easily

thankyou so much brother

tysm. I was looking for this everywhere.

thanks a lot sir god bless you it works

U r great brother nice work.

Keep going man ... Can you please help me... related topics

Thank you

Luv hogya

Well explained

Thanks sir❤

jahil aadmi yehi tu ni horaha

level yar aram se download hogya

sir your videos was awesome.Really helpful. become new subscriber please include a video about design and analysis of fins used in engines.

Part 2: kzbin.info/www/bejne/j162e2ikhchqqbM

Amazing