Transcription of ANSYS FLUENT Airfoil Analysis and Tutorial
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ANSYS FLUENT Airfoil Analysis and Tutorial
ANSYS FLUENT . Airfoil Analysis and Tutorial ENGR083: Fluid Mechanics II. Terry Yu 5/11/2017. Abstract The NACA 0012 Airfoil was one of the earliest airfoils created. Its mathematically simple shape and age have meant that it is one of the first choices for validating CFD programs, as there is a wealth of data on this particular Airfoil . Though the NACA 0012 Airfoil is not in general use currently due to its relatively poor lift to drag ratio, it remains a useful research tool. It still sees some use, however, in control surfaces and helicopter blades, as it is symmetric and thus has a simple correlation between angle of attack and lift. This project validated methods for using ANSYS FLUENT and created a Tutorial for future E83 students to also analyze this Airfoil .
May 11, 2017 · the solver is not aware of the farfield equilibrium conditions for the boundaries, and leads to waves developing in the mesh. Further investigation is required into the settings necessary to correct for this in ANSYS Fluent. We have successfully developed a tutorial to complete the lift and drag analysis on an airfoil in Fluent.
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