Numerical Investigation of Effects of Tip Clearance in Shrouded Turbine Rotor Blade Performance
Author:
Affiliation:
1. Ohio State University
2. N&R Engineering, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4437
Reference10 articles.
1. Methods of Predicting the Tip Clearance Effects in Axial Flow Turbomachinery
2. The Effect of Blade Tip Geometry on the Tip Leakage Flow in Axial Turbine Cascades
3. Rotor-Tip Leakage: Part I—Basic Methodology
4. Effect of Squealer Tip on Rotor Heat Transfer and Efficiency
5. Effects of Tip Clearance and Casing Recess on Heat Transfer and Stage Efficency in Axial Turbines
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1. THE SEALING CAPACITY AND HEAT TRANSFER CHARACTERISTICS OF A STRAIGHT-THROUGH LABYRINTH SEAL WITH DIFFERENT GEOMETRIC PARAMETERS;Heat Transfer Research;2023
2. Effect of blade tip pattern on blade load and vibration characteristics of a twin-stage axial flow fan;Journal of Mechanical Science and Technology;2022-07
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