Direct Numerical Simulations of Transitional Separation-Bubble Development in Swept-Blade Flow Conditions
Author:
Affiliation:
1. Ph.D. Candidate
2. Professor e-mail: Department of Mechanical and Aerospace Engineering, Carleton University, Ottawa, ON K1S 5B6, Canada
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4007528/6294338/turb_135_4_041006.pdf
Reference49 articles.
1. The Role of Laminar-Turbulent Transition in Gas Turbine Engines;ASME J. Turbomach.,1991
2. The Role of Transition in High-Lift Low-Pressure Turbines for Aeroengines;Prog. Aerosp. Sci.,2005
3. Instability and Transition in a Separation Bubble Under a Three-Dimensional Freestream Pressure Distribution;ASME J. Turbomach.,2012
4. Large-Eddy Simulation of Boundary-Layer Separation and Transition at a Change of Surface Curvature;J. Fluid Mech.,2001
5. Separated Flow Transition Mechanism and Prediction With High and Low Freestream Turbulence Under Low Pressure Turbine Conditions,2004
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