Work

In-depth analysis of flow field aerodynamic mechanism in integrated combustor–turbine structure for heavy-duty gas turbine

Year: 2025

Type: article

Source: Physics of Fluids

DOI: 10.1063/5.0285759

Authors: Jinghan Zhang, Haiwang Li, Zhiyu Zhou, Yuzhu Lou, Gang Xie

Institutions: Beihang University, Tianmushan Laboratory

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

SDG: Affordable and clean energy

Open Access status: closed

Funder: National Natural Science Foundation of China

Awards: G3058626230, G4610335700, G6017181851

OpenAlex ID: W4413935685

FWCI:

Cites: 29

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Related to: 10