Flow control via synthetic jet actuation

An experimental investigation was undertaken to determine the ability of Synthetic Jet Actuators to control the aerodynamic properties of a wing. The Synthetic Jet Actuator (SJA) was placed at two separate positions on a wing comprised of a NACA0015 airfoil. The first of the jet positions is located...

Full description

Bibliographic Details
Main Author: Miller, Adam Cole
Other Authors: Rediniotis, Othon
Format: Others
Language:en_US
Published: Texas A&M University 2005
Subjects:
Online Access:http://hdl.handle.net/1969.1/1409