A Refined Model to Predict Boundary of Instability of Axial Compressors
Year: 2024
Type: article
Source: Journal of Propulsion and Power
DOI: 10.2514/1.b39596
Authors: Xuegao Wang, Baofeng Tu, Jun Hu, Xinqian Zheng
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Award: G2695727732
OpenAlex ID: W4405795684