Atmospheric Test and Numerical Models Assessment of Annular Combustor on ZK2000 Gas Turbine
2018-12
发表期刊JOURNAL OF THERMAL SCIENCE
ISSN1003-2169
卷号27期号:6页码:516-526
发表状态已发表
DOI10.1007/s11630-018-1018-z
摘要ZK2000 is a newly developed 2 MW all radial gas turbine with an annular combustor. In this paper, the authors present the atmospheric test results of the combustor on test rig. Evaluation of several RANS turbulence models and reaction models were used in order to determine which model was the most appropriate combination for comparison with the test results. FGM with SST were selected because of the better agreement with test results in terms of combustor temperature rise, primary zone temperature, liner metal temperature, and NOx emission predictions.
关键词lean premixed annular combustor low emission atmospheric test flamelet generated manifold
收录类别SCI ; SCIE ; EI ; CSCD
语种英语
资助项目National Natural Science Foundation of China[51306199]
WOS研究方向Thermodynamics ; Engineering
WOS类目Thermodynamics ; Engineering, Mechanical
WOS记录号WOS:000448839000002
CSCD记录号CSCD:6350879
出版者SPRINGER
WOS关键词FLAMELET-GENERATED MANIFOLDS ; POWER-SYSTEM ; SIMULATION
原始文献类型Article
引用统计
文献类型期刊论文
条目标识符https://kms.shanghaitech.edu.cn/handle/2MSLDSTB/28302
专题物质科学与技术学院_博士生
物质科学与技术学院_特聘教授组_黄伟光组
通讯作者Gao Chuang
作者单位
1.Chinese Acad Sci, Shanghai Adv Res Inst, Shanghai 201210, Peoples R China
2.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
3.ShanghaiTech Univ, Shanghai 201210, Peoples R China
4.Helan Turbines Co Ltd, Shanghai 210815, Peoples R China
第一作者单位上海科技大学
推荐引用方式
GB/T 7714
Wang Weihao,Huang Weiguang,Cao Yun,et al. Atmospheric Test and Numerical Models Assessment of Annular Combustor on ZK2000 Gas Turbine[J]. JOURNAL OF THERMAL SCIENCE,2018,27(6):516-526.
APA Wang Weihao,Huang Weiguang,Cao Yun,&Gao Chuang.(2018).Atmospheric Test and Numerical Models Assessment of Annular Combustor on ZK2000 Gas Turbine.JOURNAL OF THERMAL SCIENCE,27(6),516-526.
MLA Wang Weihao,et al."Atmospheric Test and Numerical Models Assessment of Annular Combustor on ZK2000 Gas Turbine".JOURNAL OF THERMAL SCIENCE 27.6(2018):516-526.
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