Numerical simulation of the flow field in a single annular concentric staged combustor
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Numerical simulation of the flow field in a single annular concentric staged combustor
Vol. 25, Issue 6, (2010)
作者机构:
1. 中国航空工业集团公司 沈阳发动机设计研究所,沈阳,110015
2. 北京航空航天大学 能源与动力工程学院,北京,100191
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Published:2010
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LIU Dian-chun, DONG Yu-xi, SHANG Shou-tang, et al. Numerical simulation of the flow field in a single annular concentric staged combustor[J]. 2010, 25(6).
DOI:
LIU Dian-chun, DONG Yu-xi, SHANG Shou-tang, et al. Numerical simulation of the flow field in a single annular concentric staged combustor[J]. 2010, 25(6).DOI:
Numerical simulation of the flow field in a single annular concentric staged combustor
Influences of swirler parameters for a single annular concentric staged(SACS) combustor on non-reacting flow field in the SACS combustor were investigated computationally using standard k-εmodel.The computational results indicate that
the influences of swirling directions of the pilot swirlers on the flow field in the SACS combustor are insignificant.Influences of outer swirler on the flow field in the SACS combustor are significant when the vane angles of the three swirlers in the SACS are adjusted.Therefore
the outer swirler is a key factor to the flow structure forming in the SACS combustor.