航空科学技术Issue(6)：9-13,5.
引射喷管流量及推力特性数值研究
Numerical Investigation on Mass-lfow and Thrust Performance of the Ejector-nozzle
邓文剑 1代瑛 1王家启1
作者信息
- 1. 中航工业第一飞机设计研究院，陕西 西安 710089
- 折叠
摘要
Abstract
Several proposals were designed to investigate the thrust and mass-lfow performance of the ejector-nozzle, The performance was studied by Numerical method .the results point out that the performance of ejector-nozzle varies with variation of the main nozzle pressure ration and size of the pipe.关键词
引射喷管/次流流量/推力/数值模拟Key words
ejector-nozzle/lfow-rate/thrust/numerical simulation分类
航空航天引用本文复制引用
邓文剑,代瑛,王家启..引射喷管流量及推力特性数值研究[J].航空科学技术,2014,(6):9-13,5.
