Timeline for Can compressible flow solvers be used to solve incompressible flow?
Current License: CC BY-SA 3.0
13 events
when toggle format | what | by | license | comment | |
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Feb 11, 2016 at 14:16 | vote | accept | Paul | ||
Feb 10, 2016 at 7:43 | answer | added | solalito | timeline score: 1 | |
Feb 10, 2016 at 6:32 | answer | added | David Ketcheson | timeline score: 1 | |
Feb 10, 2016 at 5:05 | history | tweeted | twitter.com/StackSciComp/status/697285348355928064 | ||
Feb 10, 2016 at 3:12 | comment | added | tpg2114 | Track down a copy of these lecture notes for a good understanding of the math/physics in low Mach number systems and an approach for dealing with it. If you cannot find it, ping me and I will see what I can do. | |
Feb 10, 2016 at 3:10 | comment | added | tpg2114 | This is the topic of my thesis... a rough rule of thumb -- $M < 0.1$ and you are going to suffer accuracy problems with an explicit code; pressure will be under-damped numerically while momentum will be overly damped. This says nothing about efficiency. You will completely get the wrong answer at low Mach numbers and/or face numerical instabilities. | |
Feb 9, 2016 at 19:19 | answer | added | Wolfgang Bangerth | timeline score: 16 | |
Feb 9, 2016 at 16:45 | comment | added | Paul | Clearly, it would have to be in low mach regimes. Otherwise, an incompressible solver would not suffice for the same problem. | |
Feb 9, 2016 at 16:42 | comment | added | stali | Which compressible flow solvers (as in low/high mach regimes)? Also, see cs.swan.ac.uk/reports/yr2004/CSR2-2004.pdf | |
Feb 9, 2016 at 16:39 | history | edited | Paul | CC BY-SA 3.0 |
edited for brevity
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Feb 9, 2016 at 16:21 | history | edited | Paul | CC BY-SA 3.0 |
added 113 characters in body
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Feb 9, 2016 at 16:16 | history | edited | Paul | CC BY-SA 3.0 |
added 113 characters in body
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Feb 9, 2016 at 16:08 | history | asked | Paul | CC BY-SA 3.0 |