It's more than one or two results, and none of them "circumvent" the math. That is totally contradictory to what you just said. If CFD IS math, then how can a CFD case circumvent the math that created it You can calculate all day on your calculator, but if Fluent calculates no real error with the coarser mesh, who is right? Does your calculator over ride what an actual Fluent simulation says?kilcoo316 wrote:Getting one or two results on an individual study does not circumvent the maths behind it.
kilcoo316 wrote:Oh, and yes. I've seen massive differences in simulation quality going from wall function to low-Re modelling.
A disc. Great. What changes have you seen on an F1 car? I posted my result. That was an F1 front wing. And I have the Cp on the surface and I have the Cl and Cd.And even from going from a disc of 1.25 to 1.1.
Since you love math, let me talk about that. I did a richardson extrapolation on all three of those meshes, and the middle mesh was basically converged with Cp on 2 random surface points AND on Cl and Cd overall. Let me pull an excerpt from my report:
Let me explain that. The 30M cell mesh I am advocating was shown in a grid convergence study to be 0.28% off of the 4th order extrapolated value for an "infinite" cell mesh. Your glorious 120M cell fine mesh was 0.113% off the continuum mesh. Is that really worth it? Is that necessary? Is that even within the error bar of the wind tunnel, or the level of accuracy afforded by k-e or k-w? What would be the points of gaining 0.1% accuracy with your mesh when the SOLVER or turbulence models are only 2% accurate?Perhaps even more interesting is their level of accuracy with respect to the absolute converged values provided by the Richardson extrapolation. The results for the coarse, baseline, and fine grids are each within 1.79, 0.28, and 0.113 percent of the continuum (zero cell size/infinite cell).
Mate, you are TALKING about results on a disc and I am SHOWING results on F1 geometries. Which is more relevant to F1 solutions?
Using a case which couldn't be tested in the wind tunnel, did not use symmetry, and was a FORENSIC TROUBLESHOOTING application of CFD and NOT a DESIGN PROBLEM is not valid. Forensic trouble shooting is nowhere near the majority of teams' CFD cases. 100M cells is not that common.
That's why I did the extrapolation and checked the convergence of Cp, Cl, and CdEven with that most rudimentary method of comparison (the pretty picture that tells very little) there are differences in your pressure zones.
You produce some graphs of pressure along various Y locations (plotting pressure against spanwise location) and you'll see proper differences.
AIAA, Reno, January 2008 I believe.Can you name the papers?
If not, just give me the conference name and location.
You can model yaw, etc. with 50-60M cells . . . still no need for "well over 100M" on design cases. That simple is a waste.SO 30 million is ok as long as you only model the most rudimentary aspects of the car and do it in conditions which are of little actual use?