dont know if anyone gives a shit but if you're stoned like me during the covid times you can watch pretty much all the latest movies on instaflixxer. I've been binge watching with my brother for the last couple of weeks :)
If you want to add the upper and lower lines of the airfoil in one text file, after the last line of co-ordinates of the upper line leave an empty line (click enter), then paste the lower line co-ordinates, but this time name the group in the first column to be '2' instead of '1', and the continue the sequence of co-ordinate points, (i.e. if the last point of the upper line is point 67, start the lower line with 68). Add the Z co-ordinate to be zeros as shown, Then save.
Thanks it was more helpful.... If upper chord start at coordinate 1,2,0 and end at 0,0,0.... numbering is 1 Lower chord should start at coordinate 0,0,0 and end at 1,2,0... (middle contains the remaining points)...numbering is 2 A separate video will be helpful for this you know
I am having some problems: after I created correctly as you shown the profile, I got an error when i create the surface. Edge joints generated: 0. How can I fix it?
i did exactly same things but i got same error again again again. i tried toplot on excel but its aslo have a problm that i coulndt find the reason. i dunno how to solve this problem
@@mustafasabeeh8893 idk, after copying the coordintaes from excell to nitepad, and then use it in the ansys the error dialoge still appear, but ill try it one more time
Fadhlurrohman Faqih I think is the error due to not coinciding the start point with the end point, try to graph it in Excel first and be sure before importing it to Ansys
A very detailed video focusing on each minute details and concepts. The best I have come across. Thanx a lot.
No bullshit tutorial. Exactly what I am looking for
wow best explanation ever thanks alot. You saved me lots of stress
Crystal clear explanation, thank you
dont know if anyone gives a shit but if you're stoned like me during the covid times you can watch pretty much all the latest movies on instaflixxer. I've been binge watching with my brother for the last couple of weeks :)
@Bentley Donald Definitely, have been watching on InstaFlixxer for since november myself =)
thank you.finally u solved co-ordinate error .no one explained this
Really good, i was trying to make it work for hours and your video combined with some forum informations that i got really helped me.
If you want to add the upper and lower lines of the airfoil in one text file, after the last line of co-ordinates of the upper line leave an empty line (click enter), then paste the lower line co-ordinates, but this time name the group in the first column to be '2' instead of '1', and the continue the sequence of co-ordinate points, (i.e. if the last point of the upper line is point 67, start the lower line with 68). Add the Z co-ordinate to be zeros as shown, Then save.
Wow thanks bro this is informative
I was looking for that. Thanks man!
Thanks it was more helpful....
If upper chord start at coordinate 1,2,0 and end at 0,0,0.... numbering is 1
Lower chord should start at coordinate 0,0,0 and end at 1,2,0... (middle contains the remaining points)...numbering is 2
A separate video will be helpful for this you know
Thank you very much its very useful
Thank you for this details
You are a crack, thanks a lot my friend... I'll donate to you when I get a better job, grettings!
thank you so much sir. your teaching was amazing
that was incredibly helpful, thank you
Thanks! This was helpful.
Great fix! Thanks!
Huge thanks to you brother...
Perfect tutorial thank you so much
Thank u thank u thank u 🙏🏼
So helpful ! Thank you
Thanks a lot for this video.
gracias funciono
Huge thank you!!
Thanks!
Thanks for sharing such content as an Iraqi engineer, I wonder why did you use the camber line coordinates whereas other tutorials did not use them?
You are welcome, This way according to Ansys manual and I preferred to share it,Thanx
Thank you 🙏
I am having some problems: after I created correctly as you shown the profile, I got an error when i create the surface. Edge joints generated: 0. How can I fix it?
i did exactly same things but i got same error again again again. i tried toplot on excel but its aslo have a problm that i coulndt find the reason. i dunno how to solve this problem
did you fix the problem?
İf you did can you explain to me how did it?
السلام عليكم استاذ اشلون اتعلم اسوي ايميل وافتح كامرة بالبتوب ارجو الرد
hello, how can i contact you please? i need your help on fluent,???
The ANSYS CFX solver exited with return code 1. No results file has been
created. .. plz plz plz tell the solution
Check it first in excel by graphing the coordinates
I did not get you sir
@@yatinchhabra623 try to draw the coordinates in Excel application and check it if the airfoil profile appears its Ok
when i try the text to colums this 1 number turns into 1 million I'm just doing what you do
"." ları "_" haline getir en başta. Sonra sütunu ikiye ayır. Sonra "_" yaptıklarını virgül yap. Muhtemelen problemin çözülür.
@@ACFadl Kardeşim teşekkür ederim noktaları virgüle çevirince halloldu
still error :(
Fadhlurrohman Faqih are you tried to invert the upper coordinates
@@mustafasabeeh8893 idk, after copying the coordintaes from excell to nitepad, and then use it in the ansys the error dialoge still appear, but ill try it one more time
@@mustafasabeeh8893 im using nacca 4418, and still error
Fadhlurrohman Faqih I think is the error due to not coinciding the start point with the end point, try to graph it in Excel first and be sure before importing it to Ansys
@@mustafasabeeh8893 thanks, ill try it