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Forum: STAR-CCM+

October 7, 2015, 21:13

Replies: 3

Bad Convergence on Complete Aircraft Analisys

Views: 2,318

Posted By arthurdiasBR

i'm using a mesh with 6.6 million cells...

i'm using a mesh with 6.6 million cells approximatelly, it is for an article in canard airplanes regarding their aerodynamics in the general aviation.
I've never dealt with cfd meshes before as so I...

Forum: STAR-CCM+

October 6, 2015, 21:04

Replies: 3

Bad Convergence on Complete Aircraft Analisys

Views: 2,318

Posted By arthurdiasBR

Bad Convergence on Complete Aircraft Analisys

I'm a new user of Star-ccm+ Trying to simulate a canard Type aircraft in the following flow:
P = 69820 Pa
T = 268.3380 K
V = 87.45556 m/s
M = 0.2663
Rho= 0.9046 kg/m³

my set...

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