The purpose of this lecture is to :

1. Export the Cp plot on airfoil from fluent.
2. Read in excel and reverse the y axis so that negative values should be on upper side and positive values on down side as usually we see in the literature.
3. Reason for doing so is that " negative Cp values are on upper side of airfoil and positive values are on lower side of airfoil". So in order to Cp plot in same way we need to reverse the Cp plot in excel.
4. In next lecture we will compare this (CFD) Cp plot with the Cp plot from NASA data.

If you want to enhance your CFD skills in ANSYS, please have a look on the following courses:

Mastering Ansys CFD (Level 1) : Designed for newbies in CFD filed with the intention of explaining each and every option in full details which you usually not find anywhere else.

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Mastering Ansys CFD (Level 1) : Designed for newbies in CFD filed with the intention of explaining each and every option in full details which you usually not find anywhere else.

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Introduction to ICEMCFD Hexa. In this coruse you will learn Hexa meshing in ICEMCFD. You will also get one bonus problem of CFD simulation of same air foil with hexa mesh created in previous section.
Course Link: https://www.udemy.com/cfd-modelling-o...