Current position: Home >> Scientific Research >> Research Projects

模拟上游尾迹干涉的低压涡轮高升力平面叶栅试验

Hits:

Leading Scientist:Baopeng Xu

Supported by:企事业单位委托科技项目

Status:延期

Supported by:中航商用航空发动机有限责任公司

Nature of Project:横向

Date of Project Approval:2014-11-18

Scheduled completion time:2021-12-31

Date of Project Initiation:2014-11-18

Date of Project Completion:2020-12-30

Pre One:压缩氢气自燃现象的数值模拟研究

Next One:透平压缩机特定介质状态方程适应性研究