Abdullah Sahin

• Post By Abdullah Sahin
• 4 months ago
• Post Type Public

Greetings,

I am doing a fluent study on the tail types that UAVs have on Fluent. After entering the mesh settings in the attached style, I added pressure-farfield as a boundary condition around the inlet, outlet and enclosure in Fluent. After selecting the turbulence model k-omega, I changed the solution method to density-based. After measuring the Y + coefficient value 134 after the first analysis, I repeated the solution accordingly. At the same time, as the flow type in the solution steering section, I first selected subsonic flow and then incompressible when I did not get a result. 

My question is, while there is a converge state when solving on the inverted-v tail, I cannot get a converge state when doing this on the T-tail. Do you have any solution suggestions about this?