Squealer Geometry Effects on Aerothermal Performance of Tip-Leakage Flow of Cavity Tips
Author:
Affiliation:
1. Peking University, 100871 Beijing, People’s Republic of China
2. University of Cambridge, Cambridge, England CB3 0DY, United Kingdom
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.B34254
Reference31 articles.
1. Comparison of Turbine Tip Leakage Flow for Flat Tip and Squealer Tip Geometries at High-Speed Conditions
2. The Tip Leakage Flow of an Unshrouded High Pressure Turbine Blade With Tip Cooling
3. Effect of Squealer Tip on Rotor Heat Transfer and Efficiency
4. Aerodynamics of Tip Leakage Flows Near Partial Squealer Rims in an Axial Flow Turbine Stage
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