Work

Optimized thermodynamic cycle design of low infrared turbofan engine with central cone film cooling system

Year: 2025

Type: article

Source: Thermophysics and Aeromechanics

DOI: 10.1134/s0869864325010238

Authors: M. Chen, H. Zhang

Institution: Nanjing University of Aeronautics and Astronautics

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

SDG: Affordable and clean energy

Open Access status: closed

OpenAlex ID: W4416593122

FWCI:

Cites: 5

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