Numerical simulation of intercooler flow path for marine gas turbine

DONG Wei; WEN Chao-zhu; ZHENG Pei-ying

Chinese

您当前的位置：

首页 >

文章列表页 >

Numerical simulation of intercooler flow path for marine gas turbine

更新时间：2026-07-07

- Numerical simulation of intercooler flow path for marine gas turbine
- Vol. 25, Issue 3, (2010)
- 作者机构：
  
  1. 上海交通大学机械与动力工程学院,上海,200240
  2. 中国航空工业集团公司沈阳发动机设计研究所,沈阳,110015
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2010
- 稿件说明：
移动端阅览
DONG Wei, WEN Chao-zhu, ZHENG Pei-ying. Numerical simulation of intercooler flow path for marine gas turbine[J]. 2010, 25(3).
DOI：

DONG Wei, WEN Chao-zhu, ZHENG Pei-ying. Numerical simulation of intercooler flow path for marine gas turbine[J]. 2010, 25(3). DOI：

摘要

借助计算流体动力学(CFD)数值模拟技术

实现了船用燃气轮机间冷器整个流路的总压损失分析.数值模拟计算中针对间冷器模块采用了等效流通面积和等效换热效果的方法

有效解决了整个流道计算间冷器建模问题.数值模拟计算结果表明

CFD数值模拟技术可以有效的分析包括间冷器在内的整个流路的流场细节

改善间冷器的流路设计.CFD数值模拟技术与间冷换热器设计技术的结合

可以有效提高船用燃气轮机间冷器整个流路的优化设计水平.

Abstract

With the aid of CFD(computational fluid dynamics)numerical simulation technology

the total pressure loss of the intercooler entire flow path for marine gas turbine was analyzed.The equivalent flow area and equivalent heat transfer methods were used in the numerical simulation

the problem of the modeling entire intercooler flow path was solved effectively.The numerical computation results indicate that the CFD numerical simulation technology can effectively analyze the details of the flow field

helping to improve the intercooler flow path design.The combination of the CFD numerical simulation technology and intercooler design technique can improve the optimal design of the intercooler entire flow path for marine gas turbine.

关键词

Keywords

references

Views

457

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Simulation method of short crack propagation in turbine disks based on crystal plasticity

Numerical simulation of internal flow field in gas generator of fire extinguishing bomb

Design and test verification of small loitering munition electric-powered propulsion system

Influence of slit type receiver holes on radial pre-swirl system

Influence of tube length on flow resistance and temperature reduction characteristics of tubed vortex reducer

Related Author

Ping ZHANG

Shan LU

Xin JING

Mao YANG

Zhongbing LUO

Rongxin ZHOU

Yunfeng LI

Kangqing DENG

Related Institution

School of Power and Energy，Northwestern Polytechnical University

Nondestructive Testing and Evaluation Laboratory， Dalian University of Technology

College of Civil Engineering， Hefei University of Technology

Key Laboratory of Aerospace Chemical Power Technology， Hubei Institute of Aerospace Chemical Techologh， China Aerospace Science and Technology Corporation，Xiangyang Hubei

Hubei Institute of Aerospace Chemistry Technology， China Aerospace Science and Technology Corporation，Xiangyang Hubei

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰