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Thanks, Tony, for this paper.
In the 2nd paragraph of the Introduction it says:
“However, although high-order accuracy is achieved within spectral macro-elements, at the element interfaces, only 𝐶0 continuity is enforced. This has two important consequences. The first consequence may be visualization of the fluid field with an imprint of the mesh, where element boundaries are visible. A second consequence is that fluxes of derivative quantities, such as viscous dissipation, are not guaranteed to be continuous between elements.”
How serious are these errors? Both consequences are undesirable, and I want to ask if there are ways to reduce/eliminate them?
For example, when I run the example case of the turbJet I can see the fluid field imprints in my visualizations – especially in the vorticity field (which is the curl (essentially the spatial derivatives) of the velocity field). The example case uses lx1=8; so would lx1=10 or lx1=12 reduce the mesh imprint problem and/or the discontinuity in the derivative based fluxes?
To use lx1=10 or 12 with the same mesh that is given, is it a simple matter of recompiling (using ./makenek) with lx1=10 (or 12) in SIZE [e.g. line 13: parameter (lx1=10)]? Or do you have to generate a new mesh entirely, or something else?
Thank you
Nadeem
From:
nek...@googlegroups.com <nek...@googlegroups.com> on behalf of Tony Zahtila <tonyz...@gmail.com>
Date: Saturday, July 13, 2024 at 11:21 AM
To: X. G. Zhou <starlig...@163.com>
Cc: Nek5000 <nek...@googlegroups.com>
Subject: Re: [nek5000] About the accuracy of the DNS study in the streamwise flow direction.
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On Jul 15, 2024, at 6:09 PM, nadeem...@cantab.net wrote:
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So, I interpret that as:
?
Thanks
Nadeem
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On Jul 15, 2024, at 8:02 PM, nadeem...@cantab.net wrote: