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Forum: FLUENT Yesterday, 11:35
Replies: 1
Views: 45
Posted By LoGaL
So, I think you need to subtract the wing so as...

So, I think you need to subtract the wing so as to get the flow domain, but the wing solid domain must still exist. Then the two body together (flow and wing) will have a interface where the CHT...
Forum: FLUENT Yesterday, 06:32
Replies: 8
Views: 1,546
Posted By nahian_masud
Hi, Could you solve the problem? I am trying...

Hi,

Could you solve the problem? I am trying something like this.
Forum: FLUENT Yesterday, 06:32
Replies: 1
Views: 45
Posted By Amsbaoc
Conjugate Heat Transfer in Shell bodies

Hello, I am doing a structural optimization of a supersonic fighter jet wing for my end of degree thesis. To do so, I need to consider the effect of aerodynamic heating to assess thermal stresses in...
Forum: FLUENT Yesterday, 04:32
Replies: 0
Views: 39
Posted By azadaqil
Unhappy Encounter with CAD Importing Problem

I've used fluid flow (meshing with fluent) in Workbench 2024 R1. Using SpaceClaim as the platform to design my model. While using the Watertight Geometry workflow, I encountered a problem with...
Forum: Fluent UDF and Scheme Programming Yesterday, 03:59
Replies: 0
Views: 47
Posted By Chhotelal1234
Floting point expection after simulating case and data file

Dear expert,
could you please tell me why the floating point exceptional problem is occurring while I read the after-timesteps case and data file?
I am solving the 2D case with the UDF function...
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