Numerical Investigation of Tip Bifurcation on Aerodynamic Characteristics and Flow Field Structure in a Compressor Cascade

Author:

Xu Wenfeng,Mi Hanqin,Li Ao,Ren Guozhe,Lu Wenxin,Sun Dan

Publisher

Elsevier BV

Reference28 articles.

1. Influence of flow coefficient, stagger angle and tip clearance on tip vortex in axial compressor;Yoon;J. Fluids Eng.,2006

2. Vortical characteristics of the corner separation flow in a high-speed compressor cascade;Wang,2022

3. Flow control of hub corner stall in a highly loaded axial compressor cascade;Zhang;International Journal of Heat and Fluid Flow,2019

4. Pulsed suction towards unsteady active flow control in an axial compressor cascade including clearance leakage effects;Chen;Applied Thermal Engineering,2023

5. Effect of a Bionic Blade Rib on the Loss Characteristics of a Highly Loaded Compressor Cascade;Guo;Aerospace Science and Technology,2024

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