Detection of Laminar Flow Separation and Transition on a NACA-0012 Airfoil Using Surface Hot-Films
Author:
Affiliation:
1. e-mail:
2. Department of Mechanical and Aerospace Engineering, Royal Military College of Canada, Kingston, Ontario K7K 7B4, Canada
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/doi/10.1115/1.4024807/6188669/fe_135_10_101104.pdf
Reference23 articles.
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2. Control of Low Airfoil Aerodynamics;AIAA J.,1990
3. Low Speed Single Element Airfoil Synthesis,1980
4. Self-Sustained Aeroelastic Oscillations of a NACA 0012 Airfoil at Low-to-Moderate Reynolds Numbers;J. Fluids Struct.,2008
5. Aerodynamics of Laminar Separation Flutter at a Transitional Reynolds Number;J. Fluids Struct.,2010
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