Experimental investigation of the bending clearance on the aerodynamic performance in turbine blade tip region-Reference-Cited by-同舟云学术

Experimental investigation of the bending clearance on the aerodynamic performance in turbine blade tip region

Published:2020-04 Issue: Volume:197 Page:117234
ISSN:0360-5442
Container-title:Energy
language:en
Short-container-title:Energy

Author:

Shuai Jiang,Jianyang Yu,Hongwu Wang,Fu Chen,Shaowen Chen,Yanping Song

Funder

China Postdoctoral Science Foundation

Publisher

Elsevier BV

Subject

General Energy,Pollution,Mechanical Engineering,Building and Construction,Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Civil and Structural Engineering

Reference25 articles.

1. Loss mechanisms in turbomachines;Denton;J Trans Asme J Turbomach,1993

2. The measurement and formation of tip clearance loss;Bindon;J Turbomach-Trans The ASME,1989

3. Axial Turbine Tip Desensitization by Injection From a Tip Trench. Part 1: Effect of Injection Mass Flow Rat;Rao,2004

4. Axial Turbine Tip Desensitization by Injection From a Tip Trench. Part 2: Leakage Flow Sensitivity to Injection Location;Rao,2004

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

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