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January 27, 2011, 02:42 |
mesh examination
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#1 |
New Member
karthik
Join Date: Jan 2011
Posts: 2
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Hi Friends,
I'm quite new to fluent and Gambit. If any one who are good in meshing, please check my mesh quality and the details are given below Naca0012 Total no. of cells=17,000 Solver=pressure based Turbulence model= SA mach= 0.15 aoa = 0 to 16 air at standard atmospheric conditions my problem is that i compared my results(cl & cd), cl is quite good with the exprimental value but drag value differs much from experimental. please could any one help me, how to get good ci & cd... please reply me as soon as possible... thank you, karthik |
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