Numerical investigation of active tip-clearance control through tip cooling injection in an axial turbine cascade
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-009-0306-z.pdf
Reference13 articles.
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3. Li Wei, Qiao Weiyang, Sun Dawei. Tip clearance flows in turbine cascades. Chinese Journal of Aeronautics. 2008. 21: 193–199
4. Saha A K, Acharya S, Bunker R. Blade tip leakage flow and heat transfer with pressure-side winglet. International Journal of Rotating Machinery. 2006:1–15
5. Sang W L, Byoung J C. Effects of squealer rim height on aerodynamic losses downstream of a high-turning turbine rotor blade. Experimental Thermal and Fluid Science. 2008. 32: 1440–1447
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1. Control of Tip Leakage in a High-Pressure Turbine Cascade Using Tip Blowing;Journal of Turbomachinery;2017-02-07
2. Impact of Cooling Injection on the Transonic Over-Tip Leakage Flow and Squealer Aerothermal Design Optimization;Journal of Engineering for Gas Turbines and Power;2015-06-01
3. Control of Tip Leakage Vortex Breakdown by Tip Injection in Unshrouded Turbines;Journal of Propulsion and Power;2014-11
4. Reduction of turbine tip clearance losses at design and off-design incidences by non-uniform tip injection;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2014-07-08
5. Aero-thermal performance improvements of unshrouded turbines through management of tip leakage and injection flows;Energy;2014-05
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