Effects of Splitter Plates on Turbulent Quantities on a Boundary Layer Developing on a Flat Plate near the Trailing Edge-Reference-Cited by-同舟云学术

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Effects of Splitter Plates on Turbulent Quantities on a Boundary Layer Developing on a Flat Plate near the Trailing Edge

Published:2011 Issue:783 Volume:77 Page:2133-2142
ISSN:0387-5016
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
language:en
Short-container-title:Trans.JSME, Ser.B

Author:

JODAI Yoshifumi¹,ICHIMIYA Masashi,OSAKA Hideo

Affiliation:

1. Department of Mechanical Engineering, Kagawa National College of Technology

Publisher

Japan Society of Mechanical Engineers

Subject

Mechanical Engineering,Condensed Matter Physics

Link

http://www.jstage.jst.go.jp/article/kikaib/77/783/77_783_2133/_pdf

Reference13 articles.

1. The Effects of Splitter Plates on Turbulent Boundary Layer on a Long Flat Plate Near the Trailing Edge

2. The Effects of Splitter Plates on the Vortex Structure behind a Long Flat Plate with a Blunt Trailing Edge

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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