On the Unsteady Aerodynamics of a High-Speed Turbine with Squealer Blade Tips
Author:
Affiliation:
1. von Kármán Institute for Fluid Dynamics
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4434
Reference24 articles.
1. Pressure Distributions in the Tip Clearance Region of an Unshrouded Axial Turbine as Affecting the Problem of Tip Burnout
2. Jet Propulsion
3. Loss Mechanisms in Turbomachines
4. Effect of vane-rotor interaction on the unsteady flowfield downstream of a transonic high pressure turbine
5. Aerothermal Investigations of Tip Leakage Flow in Axial Flow Turbines—Part I: Effect of Tip Geometry and Tip Clearance Gap
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1. A Novel Vortex Identification Technique Applied to the 3D Flow Field of a High-Pressure Turbine;Journal of Turbomachinery;2020-02-20
2. Design and Testing of a Miniaturized Five-Hole Fast Response Pressure Probe With Large Frequency Bandwidth and High Angular Sensitivity;Journal of Engineering for Gas Turbines and Power;2019-09-13
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