I have done my airfoil related simulation in ANSYS Fluent. I want to plot a graph of lift & drag coefficient. I know how to calculate the integral values of forces and momentums over an airfoil surface. But I can't obtain a plot from it. There is no fixed variable like "drag force" or "lift force" in Tecplot variable database. Though I want to write an equation of drag or lift coefficient, I can't find all unique variable in that "Calculate variable" database.
Dear Mohammed,
I most heartily recommend
://core.ac.uk/download/pdf/74409751.pdf
With respect
Dušan
Hello Mohammad !
I don't know if I understand your question clearly or not, but i think you can use Monitors in Fluent to calculate, plot and write Lift and Drag Coefficients into a text file. For tecplot 360, Fluent is able to export tecplot files in a FEBLOCK format, however, you can load .cas and .dat files directly using "Tecplot ANSYS FLUENT"data loader.
And don't forget to check the time nature in tecplot through "Edit Time Strands" feature.
Regards,
Saad Najeeb Yes i can. But for a upcoming research paper, i have collected all graph by using Tecplot.
Ahmed Hossam El-Din i have already loaded .cas and .dat file. And i have also checked the time nature in Tecplot through "Edit Time Strands" feature. Thanks a lot for your suggestions.
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