Numerical investigation of the effects of discrete guide vanes on the control of heat transfer on the tip surface of a turbine blade

Author:

Choi Seok Min,Jung Eui Yeop,Chung Heeyoon,Cho Hyung Hee

Funder

Korea Institute of Energy Technology Evaluation and Planning (KETEP)

Korea government Ministry of Trade, Industry and Energy

Korean Institute of Energy Technology Evaluation and Planning (KETEP)

Korean Ministry of Knowledge Economy

Publisher

Elsevier BV

Subject

General Engineering,Condensed Matter Physics

Reference24 articles.

1. Heat transfer and flow on the squealer tip of a gas turbine blade;Azad;J Turbomach,2000

2. Heat transfer coefficients on the squealer tip and near squealer tip regions of a gas turbine blade;Kwak;J heat Transf,2003

3. Heat transfer coefficients on the squealer tip and near tip regions of a gas turbine blade with single or double squealer;Kwak,2003

4. Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade;Kwak;Int J Heat Mass Transf,2004

5. Effect of blade tip geometry on tip flow and heat transfer for a blade in a low speed cascade;Saxena,2003

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