Release Time:2024-01-09 Hits:
Date of Publication: 2022-10-04
Journal: 中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议
Institution: 能源与动力学院
Prev One:Unsteady study on the performance in a low-pressure turbine stages with tip clearance under design and off-design load conditions
Next One:串列叶栅扩压器第一列叶片出口角对性能的影响