相对运动条件下切量对涡轮叶片叶尖泄漏流动及气膜冷却效果的影响

IF 0.7 4区工程技术 Q4 ENGINEERING, AEROSPACE

Transactions of the Japan Society for Aeronautical and Space Sciences Pub Date : 2021-01-01 DOI:10.2322/tjsass.64.293

F. Cheng, Jing-zhou Zhang, Jingyang Zhang, Yuyan Zhang

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引用次数: 1

摘要

1)南京林业大学机电工程学院，南京210037 2)中航南京飞机系统工程研究所，南京211106 3)南京航空航天大学能源与动力工程学院，江苏省航天动力系统重点实验室，南京210016 4)航空机电系统集成航空科技重点实验室，南京2111065)南京航空航天大学航天学院，江苏南京210016

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Effect of Cutbacks on Tip Leakage Flow and Film-Cooling Effectiveness of a Turbine Blade Tip under Relative Moving Condition

1)College of Mechanical and Electronic Engineering, Nanjing Forestry University, Nanjing 210037, China 2)AVIC Nanjing Engineering Institute of Aircraft Systems, Nanjing 211106, China 3)Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China 4)Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration, Nanjing 211106, China 5)College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

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来源期刊

Transactions of the Japan Society for Aeronautical and Space Sciences 工程技术-工程：宇航

CiteScore

1.80

自引率

0.00%

发文量

审稿时长

>12 weeks

期刊介绍： Information not localized