Crossflow stability and transition experiments in a swept-wing flow

An experimental examination of crossflow instability and transition on a 45° swept wing is conducted in the Arizona State University Unsteady Wind Tunnel. The stationary-vortex pattern and transition location are visualized using both sublimating-chemical and liquid-crystal coatings. Extensive hot-w...

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Bibliographic Details
Main Author: Dagenhart, J. Ray
Other Authors: Engineering Mechanics
Format: Others
Language:en
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/39084
http://scholar.lib.vt.edu/theses/available/etd-08082007-115052/