About this document
Turbulence Effects on NACA 0015 Airfoil by koulliredouane is a document available to read on EtoBox.
This document presents an experimental study on the effects of grid-generated turbulence and continuous jet on the aerodynamic performance of the NACA 0015 airfoil. The findings indicate that increased turbulence levels and blowing velocities lead to a decrease in drag coefficient and an increase in lift coefficient by approximately 100%. The study utilizes a closed circuit wind tunnel and various experimental setups to analyze flow behavior and pressure distributions at different angles of attack.
- Author
- koulliredouane
- Language
- EN