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November 28, 2024 at 7:11 am
venkyvenkatesh374
SubscriberDear All., Basically am working on a project determining drag and lift coefficient of an aerfoil at different angle of attacks.Â
One way to change angle is by giving x and y components on velocity at inlets.Â
 Other way is to rotate the coordinate frame to the desired angle, and providing velocity normal to boundary. Am able to create a refrence frame at desired angle, but dont know how/where to set this frame to solve the case. by default fluent is considering global reference frame. ( IN CFX its easy, theres an option to set user defined frame to solve case).
Please help me to figure this out. enclosed snip of a new coordinate frame created.
Â
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November 28, 2024 at 10:10 am
Rob
Forum ModeratorDoesn't look like it. I'd be having a very careful look at the mesh too.Â
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December 5, 2024 at 5:51 am
venkyvenkatesh374
SubscriberHello., any replies to the above doubts.?? -
December 5, 2024 at 2:02 pm
Rob
Forum ModeratorYes.Â
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December 5, 2024 at 2:32 pm
venkyvenkatesh374
Subscribercan yu explain how to set a new coordinate frame to solve the case sir.
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December 5, 2024 at 2:47 pm
Rob
Forum ModeratorIt doesn't look like you can, hence my comment.Â
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