首页 | 本学科首页   官方微博 | 高级检索  
     检索      

三维加力燃烧室两相湍流燃烧的数值模拟
引用本文:章诚,叶桃红,陈义良,何家德,赵周兵.三维加力燃烧室两相湍流燃烧的数值模拟[J].航空动力学报,2000,15(4):397-400.
作者姓名:章诚  叶桃红  陈义良  何家德  赵周兵
作者单位:1. 中国科学技术大学,热科学和能源工程系,安徽,合肥,230026
2. 中国燃气涡轮研究院,四川,成都,610500
摘    要:本文对涡扇发动机三维加力燃烧室内的两相湍流燃烧过程进行了数值模拟.两相流模型采用双流体模型,湍流模型采用标准k-ε模型,湍流燃烧采用涡旋破碎(EBU) 模型,数值方法采用LEAGAP算法.计算结果定性合理.

关 键 词:加力燃烧室  两相流  燃烧  数值模拟
收稿时间:1999/9/24 0:00:00
修稿时间:1999-09-24

Numerical Simulation of Two-Phase Turbulent Combustion in a 3-D Afterburner
ZHANG Cheng,YE Tao-hong,CHEN Yi-liang,HE Jia-de and ZHAO Zhou-bing.Numerical Simulation of Two-Phase Turbulent Combustion in a 3-D Afterburner[J].Journal of Aerospace Power,2000,15(4):397-400.
Authors:ZHANG Cheng  YE Tao-hong  CHEN Yi-liang  HE Jia-de and ZHAO Zhou-bing
Institution:Department of Thermal Science and Energy Engineering,Univniversity of Science and Technology of China,Hefei230026,China;Department of Thermal Science and Energy Engineering,Univniversity of Science and Technology of China,Hefei230026,China;Department of Thermal Science and Energy Engineering,Univniversity of Science and Technology of China,Hefei230026,China;China Gas Turbine Establishment,Chengdu610500,China;China Gas Turbine Establishment,Chengdu610500,China
Abstract:
Keywords:afterburners  two phase flow  combustion  numerical simulation
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号