Control of Tip Leakage Vortex Breakdown by Tip Injection in Unshrouded Turbines-Reference-Cited by-同舟云学术

Control of Tip Leakage Vortex Breakdown by Tip Injection in Unshrouded Turbines

Published:2014-11 Issue:6 Volume:30 Page:1510-1519
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Gao Jie¹,Zheng Qun¹,Dong Ping¹,Zha Xiaohui¹

Affiliation:

1. College of Power and Energy Engineering, Harbin Engineering University, 150001 Harbin, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35283

Reference34 articles.

1. Axial Turbine Blade Tips: Function, Design, and Durability

2. SchaubU. W.VlasicE.MoustaphaS. H. “Effect of Tip Clearance on the Performance of a Highly Loaded Turbine Stage,” Technology Requirements for Small Gas Turbine, AGARD CP-537, 1993, Paper 29.

3. Lecture Series 1997-01;Sjolander S. A.,1997

4. Effects of squealer rim height on aerodynamic losses downstream of a high-turning turbine rotor blade

5. Effects of Endwall Motion on the Aero-Thermal Performance of a Winglet Tip in a HP Turbine

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