julien.decharentenay wrote:Hi,
...
Meshing, boundary conditions, etc: The detailed option is +/- what was done for the KVRC challenge. Happy to discuss specific questions. I think that most of the information is available on the website, but would be happy to clarify further. I should have (and will be) looking at running standard cases for validation purposes.
Julien
I think the GIGO commentary is reflective of just a few fundamental things that you could, to some extend, address with rather minor effort. Plus, while you may be sharing a fun idea you're excited about, you have a conflict of interests if you're also promoting your own product. Sometimes that makes folks irritable, right or not.
1. How do you define "good enough" for mesh and solution convergence criteria. Based on your coarse model generation technique (showing surface gaps at the underbody for instance), your answer may be simply that you are not rigorous at all in defining either. And if that's stated, that's fine, but your lift and drag predictions would be expected to be off by more than 100% compared to the real case, and it's not going to be a consistent error that can be corrected, so your numbers don't mean much. Also, the serious aero people will stop being interested at this point, and there's nothing wrong with that either. We know this is a $10-$40 answer, and that's not enough to buy an hour of anybody's time, so selling a nice CFD-based picture for $10-$40 is a fine enough business. But if that's the product, consider calling it something that implies a CFD-based picture rather than a CFD analysis.
2. If you have a reasonable criteria for (1), how do you model boundary conditions and so forth. Do you have a moving floor, how far does your mesh extend outward in all directions, etc. At a conceptual level, what is your black box assuming besides the specified parameters.
3. Show some honest typical results compared to public domain wind tunnel tests or validated CFD runs, and help people understand what they will be buying based on what they send you. Even NACA airfoils would be a start. Run a bunch of cases, and ideally, show us that you're always within a factor of 3. Because hey, that's an order of magnitude answer, and for $10-$40, that's something.
When you call this a CFD analysis, that generally implies it is validated, converged, etc. On the surface, this process doesn't appear to be robust enough to demonstrate that. That's why the comments sound negative - missed expectations. And if on the other hand this product provides an order of magnitude answer with real consistency - which it may do - put together some simple data to demonstrate that fact and then take full credit for everything it is and everything it isn't - the price is so low that it would be an interesting product to the right audience! After you've done this, you'll get a warmer reception, and you should still expect additional constructive criticism to help you further improve the product.
And, just in case this had a negative tone, the results you produced do look cool. Thanks for sharing.