-
-
November 28, 2024 at 7:11 amvenkyvenkatesh374Subscriber
Dear 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
-
November 28, 2024 at 10:10 amRobForum Moderator
Doesn't look like it. I'd be having a very careful look at the mesh too.Â
-
December 5, 2024 at 5:51 amvenkyvenkatesh374SubscriberHello., any replies to the above doubts.??
-
December 5, 2024 at 2:02 pmRobForum Moderator
Yes.Â
-
December 5, 2024 at 2:32 pmvenkyvenkatesh374Subscriber
can yu explain how to set a new coordinate frame to solve the case sir.
-
December 5, 2024 at 2:47 pmRobForum Moderator
It doesn't look like you can, hence my comment.Â
-
- You must be logged in to reply to this topic.
- error udf
- Help: About the expression of turbulent viscosity in Realizable k-e model
- Unburnt Hydrocarbons contour in ANSYS FORTE for sector mesh
- Fluent fails with Intel MPI protocol on 2 nodes
- Cyclone (Stairmand) simulation using RSM
- Diesel with Ammonia/Hydrogen blend combustion
- Non-Intersected faces found for matching interface periodic-walls
- Mass Conservation Issue in Methane Pyrolysis Shock Tube Simulation
- Encountering Error in Heterogeneous Surface Reaction
- How to obtain axial and tangential velocity in CFX-post?
-
1156
-
488
-
481
-
225
-
201
© 2024 Copyright ANSYS, Inc. All rights reserved.