Effects of Splitter Plates on Turbulent Quantities on a Boundary Layer Developing on a Flat Plate near the Trailing Edge
Author:
Affiliation:
1. Department of Mechanical Engineering, Kagawa National College of Technology
2. Faculty of Engineering, The University of Tokushima
3. Faculty of Engineering, Hiroshima Institute of Technology
Publisher
Japan Society of Mechanical Engineers
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://www.jstage.jst.go.jp/article/jfst/6/4/6_4_587/_pdf
Reference13 articles.
1. (1) Jodai, Y., Takahashi, Y., Ichimiya, M. and Osaka, H., The Effects of Splitter Plates on Turbulent Boundary Layer on a Long Flat Plate Near the Trailing Edge, Transactions of the ASME-Journal of Fluids Engineering, Vol. 130, No. 5(2008), CIDs 051103 (7 pages).
2. The Effects of Splitter Plates on the Vortex Structure behind a Long Flat Plate with a Blunt Trailing Edge
3. Similarities in Pressure Distribution in Separated Flow Behind Backward-Facing Steps
4. Behavior of Separated and Reattaching Flow Formed over a Backward Facing Step.
5. (5) Sato, J. and Sunada, Y., Experimental Research on Blunt Trailing-Edge Airfoil Sections at Low Reynolds Numbers, AIAA Journal, Vol. 33, No. 11(1995), pp. 2001-2005.
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