Experimental test of a compressor cascade with non-axisymmetric end-wall contouring at off-design conditions
Author:
Publisher
Elsevier BV
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology,Fluid Flow and Transfer Processes,Mechanical Engineering
Reference28 articles.
1. Loss Mechanisms in Turbomachines;Denton,1993
2. Experimental test of a 3D parameterized vane cascade with non-axisymmetric endwall;Guo;Aerosp. Sci. Technol.,2019
3. A simultaneous use of a leading-edge fillet and a non-axisymmetrically contoured endwall in a turbine stage;Turgut;Aerosp. Sci. Technol.,2021
4. Numerical investigation and loss estimation of high-pressure turbine cascade flow with contoured endwall and incoming wakes;Hu;Aerosp. Sci. Technol.,2020
5. Loss reduction in a high-speed compressor cascade using an L-shaped endwall groove to generate a streamwise vortex;Wang;Aerosp. Sci. Technol.,2022
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