Effect of rotation on film cooling with a single row of shaped holes on blade pressure side-Reference-Cited by-同舟云学术

Effect of rotation on film cooling with a single row of shaped holes on blade pressure side

Published:2017 Issue:2 Volume:12 Page:JTST0016-JTST0016
ISSN:1880-5566
Container-title:Journal of Thermal Science and Technology
language:en
Short-container-title:JTST

Author:

ZHU Xingdan¹,ZHANG Jingzhou¹²,TAN Xiaoming¹,SHAN Yong¹

Affiliation:

1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics

2. Collaborative Innovation Center of Advanced Aero-Engine

Publisher

Japan Society of Mechanical Engineers

Subject

Engineering (miscellaneous),Instrumentation,General Materials Science,Atomic and Molecular Physics, and Optics

Link

https://www.jstage.jst.go.jp/article/jtst/12/2/12_2017jtst0016/_pdf

Reference39 articles.

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2. Ahn, J., Schobeiri, M. T., Han, J. C. and Moon, H. K., Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint, Transactions of the ASME, Journal of Heat Transfer, Vol.128, No.9 (2006), pp.879-888.

3. Ahn, J., Schobeiri, M. T., Han, J. C. and Moon, H. K., Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes, International Journal of Heat and Mass Transfer, Vol.50, No.1-2 (2007), pp.15-25.

4. Alzurfi, N. and Turan, A., LES of rotational effects on film cooling effectiveness and heat transfer coefficient in a gas turbine blade with one row of air film injection, International Journal of Thermal Sciences, Vol.99, No.1 (2016), pp.96-112.

5. Andreopoulos, J. and Rodi, W., Experimental investigation of jets in a crossflow, Journal of Fluid Mechanics, Vol.138, No.138 (1984), pp.93-127.

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