Work

Effect of showerhead hole injection angle on film cooling distribution in a turbine vane cascade

Year: 2026

Type: article

Source: Experimental Thermal and Fluid Science

DOI: 10.1016/j.expthermflusci.2026.111826

Authors: Woojun Kim, Chan Gyu Lee, Wonseok Lim, Jin Young Jeong, Min Seok Kang, Jae Su Kwak

Institution: Korea Aerospace University

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

SDG: Affordable and clean energy

Open Access status: closed

Funders: Ministry of Trade, Industry and Energy, Gyeonggi-do Regional Research Center, Korea Institute of Energy Technology Evaluation and Planning

Awards: G5593377171, G8049830535

OpenAlex ID: W7204466738

FWCI:

Cites: 19

Cited by:

Related to: 10