Work

Influence mechanism of advance ratio on the aerodynamic performance of a contra-rotating propfan

Year: 2025

Type: article

Source: International Journal of Turbo and Jet Engines

DOI: 10.1515/tjj-2025-0089

Authors: Cao Zhiyuan, Gu Qinpeng, Guo Wei, He Xiang, Peng Xuemin, Liu Bo

Institutions: Northwestern Polytechnical University, Aero Engine Corporation of China (China)

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4414414434

FWCI:

Cites: 16

Cited by:

Related to: