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September 28, 2014, 05:57 |
wall Y plus
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#1 |
Member
tahir
Join Date: May 2010
Posts: 35
Rep Power: 15 |
I am doing external CFD on irregular body. I have to solve Mach number above 1 and less than 1. I am confuse in wall Y plus. what value should i achieve for subsonic and supersonic flow. can anybody guide me
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September 28, 2014, 06:14 |
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#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
Subsonic/supersonic is irrelevant for y+ selection. What is important is whether you need to resolve down to the viscous sublayer or not.
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September 28, 2014, 06:38 |
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#3 |
Member
tahir
Join Date: May 2010
Posts: 35
Rep Power: 15 |
Thanks for reply. Glenn if i resolve the viscous sublayer then will i get my results more accurate
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September 29, 2014, 06:25 |
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#4 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
What results are you trying to get?
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September 29, 2014, 10:17 |
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#5 |
Member
tahir
Join Date: May 2010
Posts: 35
Rep Power: 15 |
gelnn in first phase i will find Cd, Cl and pitching moment coefficient. Then in second phase i will find rolling coefficient
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October 5, 2014, 07:43 |
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#6 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
It depends on what you are modelling. This conversation is becoming circular.
I would recommend reading a text book on turbulence modelling, such as "Turbulence Modelling for CFD" by Wilcox. You really need a bit of background in these areas so you can understand the implications of your modelling choices. |
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