Modeling Transition in Separated and Attached Boundary Layers
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Carleton University, 3135 Mackenzie Building, 1125 Colonel By Drive, Ottawa, ON K1S 5B6, Canada
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/127/2/402/6837344/402_1.pdf
Reference67 articles.
1. The Laminar-Turbulent Transition in a Boundary Layer—Part I;Emmons;J. Aeronaut. Sci.
2. Schubauer, G. B., and Skramstad, H. K., 1948, “Laminar Boundary-Layer Oscillations and Transition on a Flat Plate,” NACA TN 909.
3. Natural Transition of Boundary Layers: The Effects of Turbulence, Pressure Gradient and Flow History;Abu-Ghannam;J. Mech. Eng. Sci.
4. The Origin of Turbulent Spots;Johnson;ASME J. Turbomach.
5. Three-dimensional Receptivity of Boundary Layers;Kachanov;Eur. J. Mech. B/Fluids
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