Work

Investigation on the Blade Leading-Edge Film Cooling With Normal and Staggered-Oblique Impinging Jets

Year: 2026

Type: article

Source: Journal of Turbomachinery

DOI: 10.1115/1.4070875

Authors: Li Hongye, Xu Qingzong, Wang Shanyou, Xu Jiawei, Xu Guangyao, Liu Haoyang, Du Qiang, Zhu Junqiang

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: G7821668069

OpenAlex ID: W7124132907

FWCI: 2.933

Cites: 40

Cited by: 1

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