![]() ![]() ![]() Also, we selected the maximum speed of 20.78736m/s for the inlet. In the present case, the angle of attack is 16 degrees and the length of the chord and the width of the airfoil are assumed to be equal to 1. The purpose of this paper is to investigate the behavior of airflow and pressure distribution, as well as to study drag and lift forces. The direction of the airflow into the body is defined by the angle of attack (the angle between the chord and the horizontal direction of the airflow velocity). Geometric defining parameters include chord line, angle of attack, leading edge, and trailing edge. This project is going to simulate a NACA 0008 Airfoil in the airflow field with ANSYS Fluent software. Civil & Hydraulic Structures EngineeringÄescription Airflow Around a NACA 0008 Airfoil CFD Simulation, ANSYS Fluent Training Description. ![]()
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