Effect of radial inlet distortion on aerodynamic stability in a high load axial flow compressor
Year: 2024
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0235393
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G2214616499, G4425255896, G6639175728
OpenAlex ID: W4403541110
