Loading Distribution Effects on Separated Flow Transition of Ultra-High-Lift Turbine Blades
Author:
Affiliation:
1. Department of Mechanical, Energy, Management and Transportation Engineering (DIME), University of Genoa, 16145 Genoa, Italy
2. Avio Aero, 10010 Torino, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34968
Reference44 articles.
1. The 1991 IGTI Scholar Lecture: The Role of Laminar-Turbulent Transition in Gas Turbine Engines
2. An assessment of the laminar kinetic energy concept for the prediction of high-lift, low-Reynolds number cascade flows
3. A Combined Experimental/Numerical Study of Unsteady Phenomena in a Laminar Separation Bubble
4. Transition Mechanisms in Separation Bubbles Under Low- and Elevated-Freestream Turbulence
5. Large-eddy simulation of boundary-layer separation and transition at a change of surface curvature
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