Numerical study of hole shape effect on blade cooling effectiveness

Yao, Jun and Sian, Sohan and Yao, Yufeng and Davis, Tony W. (2010) Numerical study of hole shape effect on blade cooling effectiveness. Modern Physics Letters B: Condensed Matter and Statistical Physics , 13 (24). pp. 1295-1298. ISSN 0217-9849

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Official URL: http://dx.doi.org/10.1142/S0217984910023463

Abstract

Numerical study of hole shape effect on blade adiabatic cooling effectiveness has been carried out
on four geometry models of a standard cylindrical hole, a cylindrical hole with an upstream ramp, a
shaped diffuser, and a double console slot. In all cases, the hole centerline has an inclination angle of
35 degrees against the mainstream gas flow. Results of the cylindrical hole model are in good
agreement with available experimental and numerical data. For three hole geometry variants
considered, it was found that the cooling effectiveness has been considerably enhanced by a max
factor of 2, compared to that from the base model. The physical mechanism for this is mainly due to
the weakening of coolant flow penetration in the vicinity of the hole exit, thus reduces the level of
mixing and the entrainment with the surrounding hot gas flow.

Item Type:Article
Keywords:hole shape effect, adiabatic cooling effectiveness
Subjects:H Engineering > H321 Turbine Technology
Divisions:College of Science > School of Engineering
ID Code:5424
Deposited By: Jun Yao
Deposited On:06 May 2012 23:04
Last Modified:18 Nov 2013 16:09

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