Hey guys Am new with Fluent and i am making a 2D airfoil simulation ; I ve calculated Cl Cd Cm but i still dont know how to calculate Cdp . Can you please help me with this point?
Mohammed Ba Zuhair Thank you for the video but it only explain how to plot the values of cdp . but what i want is how can i get just 1 Cdp value for the whole wing ?
As shown in the beginning of the video, the built-in function and its window are displayed, implying how to reach them easily in ANSYS Workbench Results Post-Processor ! For Fluent go to >> Results >> Plots >> Y axis function "Pressure" >> Pressure Coefficient Pressure, with desired X axis parameter.