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April 9, 2019 at 7:58 pm
acgerrard
SubscriberHi all,Â
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,Â
Alasdair
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April 10, 2019 at 6:45 am
Keyur Kanade
Ansys Employeeplease check this.Â
https://confluence.cornell.edu/display/SIMULATION/FLUENT+-+3D+Transonic+Flow+Over+a+Wing
Â
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April 10, 2019 at 9:41 am
acgerrard
SubscriberGreat, thank you!
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September 11, 2020 at 12:58 am
Karthik Remella
AdministratorThese 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 ModeratorThe Cornell course is free, so register & watch the lectures. n -
September 11, 2020 at 12:49 pm
Karthik Remella
AdministratorHello,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
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