Work

Effects of labyrinth cavity angles and non-axisymmetric end wall on the performance of the shrouded stator at different inlet boundary layer thicknesses

Year: 2025

Type: article

Source: Physics of Fluids

DOI: 10.1063/5.0286356

Authors: Hao Liu, Guoqing Li, Chenyang Kang, Yunhong Ruan, Hang Yuan, Xingen Lu

Institutions: Chinese Academy of Sciences, Institute of Engineering Thermophysics, University of Chinese Academy of Sciences

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Award: G3039563758

OpenAlex ID: W4413926966

FWCI: 0.4

Cites: 22

Cited by: 1

Related to: 10