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Old   September 28, 2014, 05:57
Default wall Y plus
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tahir
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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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Old   September 28, 2014, 06:14
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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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Old   September 28, 2014, 06:38
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Thanks for reply. Glenn if i resolve the viscous sublayer then will i get my results more accurate
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Old   September 29, 2014, 06:25
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What results are you trying to get?
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Old   September 29, 2014, 10:17
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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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Old   October 5, 2014, 07:43
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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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