Technical Report: Aerodynamic Characteristics of the NACA 0015 Airfoil 1. Abstract
The NACA 0015 exhibits a "trailing edge stall," where the flow separation begins at the rear and moves forward as the AoA increases. 5. Conclusion Download 0015 txt
) across varying angles of attack (AoA) to identify stall behavior and efficiency. 2. Introduction Download 0015 txt
The NACA 0015 is a standard benchmark in aerodynamics due to its symmetry and well-documented performance. It is frequently used in the design of aircraft vertical stabilizers, helicopter rotors, and wind turbines. The primary objective of this analysis is to validate numerical data against historical experimental results to ensure accuracy in design applications. 3. Methodology 3.1 Geometry and Profile Download 0015 txt