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Influence of Turbulence Schmidt Number on Exit Temperature Distribution of an Annular Gas Turbine Combustor using Flamelet Generated Manifold

WANG Weihao YANG Songlin GAO Chuang HUANG Weiguang

热科学学报（英文版）2020，Vol.29Issue(1)：58-68,11.

Influence of Turbulence Schmidt Number on Exit Temperature Distribution of an Annular Gas Turbine Combustor using Flamelet Generated Manifold

WANG Weihao ¹YANG Songlin ²GAO Chuang ³HUANG Weiguang⁴

作者信息

1. Shanghai Advanced Research Institute, Chinese Academy of Sciences, Shanghai 201210, China
2. University of Chinese Academy of Sciences, Beijing 100049, China
3. School of Physical Science and Technology, ShanghaiTech University, Shanghai 201210, China
4. Helan Turbines Co., Ltd, Shanghai 201815, China
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摘要

关键词

gas turbine combustor/flamelet-generated manifold/turbulent Schmidt Number/Reynolds Stress Model/Reynolds analogy

Key words

gas turbine combustor/flamelet-generated manifold/turbulent Schmidt Number/Reynolds Stress Model/Reynolds analogy

引用本文复制引用

WANG Weihao,YANG Songlin,GAO Chuang,HUANG Weiguang..Influence of Turbulence Schmidt Number on Exit Temperature Distribution of an Annular Gas Turbine Combustor using Flamelet Generated Manifold[J].热科学学报（英文版）,2020,29(1):58-68,11.

基金项目

This work is funded by the Key Programs of Chinese Academy of Sciences (Project No.ZDRW-CN-2017-2). （Project No.ZDRW-CN-2017-2）

热科学学报（英文版）

OACSCDEISCI

ISSN：1003-2169

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