Analysis of NACA 2412 Airfoil for Aerodynamic Efficiency
This research paper focuses on a small foam wing analysis using NACA 2412 airfoil. This study aims to determine the stall angle, the lift coefficient, and the stall speed through theoretical analysis. The findings are essential for understanding the aerodynamic limitations of the wing and for ensuring optimal flight performance.
Authors
- Steven Grover
Publication Details
- Journal
- International Journal for Research in Applied Science and Engineering Technology
- Published
- 2025-03-19
- DOI
- https://doi.org/10.22214/ijraset.2025.67531
- Primary Topic
- Aerospace and Aviation Technology
- Type
- article
- Field-Weighted Citation Impact
- 0.00