About this document
Nasa TP 3478 by ly-wl is a document available to read on EtoBox.
This NASA Technical Paper presents a comprehensive analysis of flow over the F/A-18 aircraft using Navier-Stokes equations, complemented by flight and wind tunnel data. The study evaluates aerodynamic performance at high angles of attack, focusing on the effects of flow separation and vortical structures on maneuverability. The results indicate strong correlations between computational and experimental data, providing insights into the aircraft
- Author
- ly-wl
- Language
- EN