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March 2, 2011, 23:46 |
Airfoil Average Nusselt Number calculation
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#1 |
New Member
Join Date: Mar 2011
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Rep Power: 15 |
Hi everyone my current version of ANSYS Fluent is 12.1
The type of flow I am using is a Spalart Allarmaras Model Please correct me if I am wrong Now, I wantwant to calculate an average nusselt number from the Solution so do I just simply click "monitor" -> " Surface Monitor" Report Type: Integral Field Variable: Wall Fluxes, Surface Nusselt Number?? and also how do I calculate the Reynolds number of the flow as well ? Thanks =) |
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March 3, 2011, 01:25 |
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#2 |
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I have the Nusselt Number Distribution around the airfoil
does the Nu Distribution look like that ? and how do I average them ? just add them all and divide by the number of point, n ??? ps: this airfoil is a unit length airfoil Thanks |
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March 3, 2011, 03:41 |
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#3 |
Senior Member
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Hi,
before computing Nu No., be sure that your reference values are correct.(report->reference values) I think for evaluating average Nu No., you can compute total heat transfer from airfoil and then obtain an equivalent h(heat transfer coefficient) and then compute Nu.(just a suggestion) |
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March 3, 2011, 04:47 |
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#4 | |
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Quote:
as far as obtaining equivalent h from total heat transfer... what delta temperature should I use ?? ( Temperature varies along the chord length too) Thanks, |
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March 3, 2011, 05:21 |
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#5 |
Senior Member
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I think it's a good idea to use dT=(Tave-Tinf). you can obtain Tave from report->surface integral->average facet. isn't it?
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March 3, 2011, 06:45 |
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#6 | |
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Quote:
h_avg = overall_heat_transfer_rate / ( T_avg - T_fluid ) Nu_avg = h_avg * chord_length / k_fluid correct me if I am wrong |
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March 3, 2011, 08:37 |
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#7 |
Senior Member
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