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...
Tallennettuna:
| Päätekijät: | , , , , , |
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| Aineistotyyppi: | Artigo |
| Kieli: | Inglês |
| Julkaistu: |
SpringerOpen
2023-09-01
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| Sarja: | Advances in Aerodynamics |
| Aiheet: | |
| Linkit: | https://doi.org/10.1186/s42774-023-00154-0 |
| Tagit: |
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