Numerical Study of Instability Mechanisms Leading to Transition in Separation Bubbles
Author:
Affiliation:
1. Aerodynamics Laboratory, Institute for Aerospace Research, 1200 Montreal Road, Building M-2, Ottawa, ON K1A 0R6, Canada
2. Department of Mechanical and Aerospace Engineering, Carleton University, 1125 Colonel By Drive, Ottawa, ON, K1S 5B6, Canada
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2750680/5680224/021006_1.pdf
Reference33 articles.
1. The Role of Laminar-Turbulent Transition in Gas Turbine Engine;Mayle;ASME J. Turbomach.
2. Roberts, S. K., and Yaras, M. I., 2003, “Effects of Periodic Unsteadiness, Free-Stream Turbulence and Flow Reynolds Number on Separation-Bubble Transition,” ASME Paper No. GT2003-38626.
3. Boundary-Layer Transition Affected by Surface Roughness and Free-Stream Turbulence;Roberts;ASME J. Fluids Eng.
4. Effects of Surface Roughness Geometry on Separation-Bubble Transition;Roberts;ASME J. Turbomach.
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