Work

The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall

Year: 2024

Type: article

Source: Journal of Turbomachinery

DOI: 10.1115/1.4067121

Authors: Shuo Mao, Kaiyuan Zhang, Daniel Van Hout, Wing F. Ng, Hongzhou Xu, Michael Fox

Institution: Virginia Tech

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4404240235

FWCI: 0.525

Cites: 33

Cited by: 3

Related to: 10