About this document
NACA 4421 Airfoil Analysis Report by Raphael Andres Rubiano Vasco is a document available to read on EtoBox.
The document is the final report of an analysis of the NACA 4421 airfoil conducted by engineering students at the European University of Madrid. It includes theoretical predictions of lift and drag coefficients for the airfoil at various angles of attack, as well as computational fluid dynamics simulations using ANSYS software to analyze velocity magnitude, velocity vectors, pressure distribution, and other characteristics of airflow over the airfoil at angles of 0, 5, 10, and 15 degrees. The results show h
- Author
- Raphael Andres Rubiano Vasco
- Language
- EN