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October 17, 2019 at 4:01 pm
roytorc
SubscriberHi,
I am modelling the turbulent non-premixed flame touching the adiabatic surface (by set heat flux of the wall =0 in thermal boundary condition). However, there is a temperature gradient near the wall which I don't understand how is that possible. I've checked the heat flux across the boundary and it is 0. Please advise.
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October 17, 2019 at 5:59 pm
DrAmine
Ansys EmployeeCheck temperature of the wall and near wall cell temperature -
October 17, 2019 at 6:27 pm
roytorc
SubscriberAfter checked, the values are:
wall --> Contour level 6, value in [820.98102, 907.81116].
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near wall cell --> Contour level 10, value in [1168.3018, 1255.1318].
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I still don't understand why there is the temperature gradient. Please help advise.
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October 18, 2019 at 4:42 am
DrAmine
Ansys EmployeeNo on the wall check the wall temperature then on the same wall the cell temperature. -
October 18, 2019 at 3:09 pm
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October 18, 2019 at 3:19 pm
DrAmine
Ansys EmployeeThat is not ideal so. You need to quantify it in better way. Either you use UDF or plot along the line wall and static temperature. -
October 18, 2019 at 3:19 pm
DrAmine
Ansys EmployeeOr look after the gradients which you enable under solve set expert. -
October 18, 2019 at 3:21 pm
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October 18, 2019 at 5:36 pm
DrAmine
Ansys EmployeeKeep temporary... to yes to see gradients for Post processing
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