Effects of the squealer winglet structures on the heat transfer characteristics and aerodynamic performance of turbine blade tip

Author:

Jiang Shijie,Li Zhigang,Li Jun

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference30 articles.

1. State-of-the-art cooling technology for a turbine rotor blade;Town;J. Turbomach.,2018

2. T.C. Booth, Importance tip clearance flows in turbine design, in: Tip Clearance Effects in Axial Turbomachines, Von Karman Institute Lectures Series, VKI LS 1985-05, 1985.

3. Axial turbine blade tips: function, design, and durability;Bunker;J. Propul. Power,2006

4. Effects of tip geometry and tip clearance on the mass/heat transfer from a large-scale gas turbine blade;Papa;J. Turbomach.,2003

5. N. Harvey, D. Newman, F. Haselbach, An Investigation into a Novel Turbine Rotor Winglet. Part I: Design and Model Rig Test Results, ASME Paper No.GT2006-90456, 2006.

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