Numerical Investigation of the Effects of ITD Length on Low Pressure NozzleOACSCD

作者：LIU Guang;LIU Jun;Liu Hongrui;Wang Pei;DU Qiang

作者单位：Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaUniversity of Chinese Academy of Sciences, Beijing, 100049, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaInstitute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China

中文关键词：Intermediate Turbine DuctLengthNozzlePressure Loss

英文关键词：Intermediate Turbine DuctLengthNozzlePressure Loss

刊名：《热科学学报：英文版》 2017 (3)

相关项目：进口预旋下一体式超紧凑高低压涡轮过渡段流场重构机理研究

页码/页数：199-207,9

基金：This research is supported by National Natural Science Foundation of China (approval serial number:51406204).

DOI：10.1007/s11630-017-0930-y