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Numerical study on the combustion process in a gas turbine combustor with different reference velocities

Abstract The mixing and combustion processes under different reference velocities in a gas turbine combustor were numerically investigated using the Flamelet Generated Manifold (FGM) model based on the Reynolds Averaged Navier–Stokes (RANS) method. The flow and combustion fields show strong self-sim...

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Principais autores: Cheng Gong, Shufan Zhao, Weiqiang Chen, Wenyu Li, Yu Zhou, Ming Qiu
Format: Artigo
Sprog:Inglês
Udgivet: SpringerOpen 2023-09-01
Serier:Advances in Aerodynamics
Fag:
Gas turbine combustor
Swirling flame
FGM
Combustion mode
Time-scale analysis
Online adgang:https://doi.org/10.1186/s42774-023-00154-0
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