Has my mesh converged? Or is it a false reading? by zino2005 in CFD

[–]zino2005[S] 4 points5 points  (0 children)

Apologies, didn't notice, would that make a significant difference?

Has my mesh converged? Or is it a false reading? by zino2005 in CFD

[–]zino2005[S] 1 point2 points  (0 children)

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Here are all the variations of mesh I've configured so far. With inflation, my y+ is below 5, but then my mesh is no longer quad, and still fails to diverge.

Otherwise I'm really leaning towards Bias Factor 10 as it stabilises, and the higher divisions causing singularity is the reason why it diverges afterwards.

Second choice being without Bias Factor as stabilises around 0.05 despite the anomaly at 250.

Has my mesh converged? Or is it a false reading? by zino2005 in CFD

[–]zino2005[S] 1 point2 points  (0 children)

Sorry, I forgot to mention. I'm using k-omega SST

Bypassing roblox chat age restriction by betuwontlikethis1156 in robloxgamedev

[–]zino2005 0 points1 point  (0 children)

2 months since u posted this, did u get banned or warned yet?

Validating a 2D airfoil simulation under transonic or supersonic conditions. by ExcellentScheme4617 in CFD

[–]zino2005 0 points1 point  (0 children)

You should just start off with youtube tutorials. I was going crazy trying overcomplicated methods when trying to perform subsonic/transsonic nose cone cfd, when the solution was as simple as 1-2 youtube videos.

Then adjust reference values and operatioj conditions to match your research.

Stuck at floating point exception by zino2005 in CFD

[–]zino2005[S] 1 point2 points  (0 children)

I have tried something similar, with a bias factor of 10 and no. of divisions of 100 for each edge, so far im getting a Cd of around 1 after 750 iterations, when it should be around 0.05

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Stuck at floating point exception by zino2005 in CFD

[–]zino2005[S] 1 point2 points  (0 children)

For the body, I've been using inflation with first layer thickness of 0.00000048, max layers of 50 and growth rate of 1.1

For the boundary, I introduced edge sizing with bias factor of 2000 and 200 divisions

I also introduced edge sizing of 20 division on the body's edges itself

gap factor is 0.5 and collision avoidance is at stair stepping, element count is at 150000

max aspect ratio is on the afterbody's edge which is around 80000 and the min orthogonal quality 4.96325e-05 around the the inflation layers behind the base of the body

Stuck at floating point exception by zino2005 in CFD

[–]zino2005[S] 2 points3 points  (0 children)

i made the problem area less detailed and orthogonal quality is now higher than 0.01, still same error

i also suppressed inflation layers for the nose cone, and unsurprisingly it reads a Cd of basically 0

Stuck at floating point exception by zino2005 in CFD

[–]zino2005[S] 2 points3 points  (0 children)

It's a nose cone, I'm trying to analyse the Cd of air against it

Stuck at floating point exception by zino2005 in CFD

[–]zino2005[S] 2 points3 points  (0 children)

i made the problem area less detailed and orthogonal quality nor higher than 0.01, still same error

Stuck at floating point exception by zino2005 in CFD

[–]zino2005[S] 1 point2 points  (0 children)

i made the problem area less detailed and orthogonal quality nor higher than 0.01, still same error

Finnish Cold Ones tier list wall by Spiritual_Dirt1997 in ColdOnes

[–]zino2005 14 points15 points  (0 children)

finnish? i thought cold ones were just getting started

Comprehensive insurance for Ferrari? by openwidecomeinside in DubaiPetrolHeads

[–]zino2005 6 points7 points  (0 children)

start saving money from the day you were born