Lift distribution across wing

- April 9, 2019 at 7:58 pm
  
  acgerrard
  Subscriber
  
  Hi all,
  
  I was wondering if there is a way to generate the lift distribution on a 3D wing in Fluent? I have attempted to get the pressure coefficient along the wing by using a plane and across the component itself. Is there a way that doesn't involve untangling all the points from the cp graph?
  
  Thanks,
  
  Alasdair
- April 10, 2019 at 6:45 am
  
  Keyur Kanade
  Ansys Employee
  
  please check this.
  
  https://confluence.cornell.edu/display/SIMULATION/FLUENT+-+3D+Transonic+Flow+Over+a+Wing
- April 10, 2019 at 9:41 am
  
  acgerrard
  Subscriber
  
  Great, thank you!
- September 11, 2020 at 12:58 am
  
  Karthik Remella
  Administrator
  
  These Cornell courses are now a part of Ansys Innovation Courses (AICs). Please take a look at this link here.nnPlease also take a look at our other Fluids courses.nThank you.n
- September 11, 2020 at 12:48 pm
  
  Rob
  Forum Moderator
  
  The Cornell course is free, so register & watch the lectures. n
- September 11, 2020 at 12:49 pm
  
  Karthik Remella
  Administrator
  
  Hello,nIf your question is how to access the Cornell tutorial for setting-up a 3D transonic flow over a wing, then this content in the link you are sharing has been moved to a new location. Here is the new location to this same Cornell content (same link that I already shared with you in my earlier post). You should be able to go through this tutorial and learn about how to model a 3D wing and generate the lift force distribution..nIf you have a specific question.please create a new post and we will be happy to help you with it.nThanks.nKarthikn