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Forum: FLUENT

October 4, 2016, 03:36

Replies: 2

NACA 0012, AOA=0, Lift=/0

Views: 1,516

Posted By Freestream

Hi everyone, i have resolved the problem by...

Hi everyone, i have resolved the problem by simply rotating the airfoil in Design Modeler, instead of resolving input velocity in the x and y direction.

the result have shown that fault lies in...

Forum: FLUENT

September 29, 2016, 23:02

Replies: 2

NACA 0012, AOA=0, Lift=/0

Views: 1,516

Posted By Freestream

Hi everyone, i have an update on the result. ...

Hi everyone, i have an update on the result.

i attempt to refined the mesh and employ SA turbulence model with coupled solution scheme. At Re=3e6

the lift coefficient results i have are as...

Forum: FLUENT

September 25, 2016, 01:15

Replies: 2

NACA 0012, AOA=0, Lift=/0

Views: 1,516

Posted By Freestream

NACA 0012, AOA=0, Lift=/0

Hi everyone,

I am a final year student in University of Glasgow doing Aeronautical Engineering. I am doing a project of numerical study on NACA 0012 in ANSYS Fluent.

I have read/watched...

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