Effect of Orientation of Internal Turbulence Promoting Ribs on Flow Characteristics for Film Cooling

Author:

AGATA Yukiko12,TAKAHASHI Toshihiko1,SAKAI Eiji1,NISHINO Koichi2

Affiliation:

1. Central Research Institute of Electric Power Industry

2. Department of Mechanical Engineering, Graduate School of Engineering, Yokohama National University

Publisher

Japan Society of Mechanical Engineers

Subject

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

Reference16 articles.

1. (1) Eriksen, V. L. and Goldstein, R. J., Heat transfer and film cooling following injection through inclined circular tubes, Transactions of the ASME, Journal of Heat Transfer, Vol.96 (1974), pp.239-245.

2. (2) Schmidt, D. L., Sen, B. and Bogard, D. G., Film Cooling With Compound Angle Holes: Adiabatic Effectiveness, Transactions of the ASME, Journal of Turbomachinery, Vol.118 (1996), pp. 807-813.

3. (3) Ekkad, S. V., Zapata, D. and Han, J. C., Film effectiveness over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method, Transactions of the ASME, Journal of Turbomachinery, Vol.119(1997), pp.587-593.

4. (4) Nasir, H., Acharya, S. and Ekkad, S., Improved film cooling from cylindrical angled holes with triangular tabs: effect of tab orientations, International journal of Heat and Fluid Flow, Vol.24(2003), pp.657-668.

5. Evolution of jets emanating from short holes into crossflow

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