Work

Response and stall mechanism for axial compressor under rotating inlet distortion

Year: 2025

Type: article

Source: Physics of Fluids

DOI: 10.1063/5.0254496

Authors: Shuai Ma, Zhiqiang Wang, Jun Hu

Institution: Nanjing University of Aeronautics and Astronautics

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4407136132

FWCI: 1.998

Cites: 22

Cited by: 5

Related to: 10