Experimental Investigation of Boundary Layer Separation
Publisher
The University of Arizona.Rights
Copyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction, presentation (such as public display or performance) of protected items is prohibited except with permission of the author.Abstract
A study of boundary layer separation in wind tunnel, water tunnel, and free-flight conditions is reported on within these pages. Methods and results for building a sub-scale wing glove, installing active flow control, and testing in flight are presented. Water tunnel dye flow visualizations and particle image velocimetry of laminar separation bubbles are also presented.Type
textElectronic Thesis
Degree Name
M.S.Degree Level
mastersDegree Program
Graduate CollegeAerospace Engineering