About this document
NACA 4415 Wing Performance Analysis by 222nikhilkumar is a document available to read on EtoBox.
The document details a series of practical experiments conducted on a NACA 4415 wing, including performance estimation, CFD analysis, and static structural analysis. Results indicate a lift coefficient of approximately 0.717 and a drag coefficient of 0.086 from hand calculations, while CFD results showed lower values due to three-dimensional effects. The structural analysis revealed safety factors below 1, suggesting the need for redesign to prevent yielding under the applied aerodynamic loads.
- Author
- 222nikhilkumar
- Language
- EN