Investigation on the Mechanism of Blade Tip Recess Improving the Aerodynamic Performance of Transonic Axial Flow Compressor
The development of high-performance aero engines put forward higher performance requirements for compressor components, and the improvement of aerodynamic performance of compressors has important engineering application value. The blade tip recess has great potential and advantages in improving the...
| मुख्य लेखकों: | , , , , , |
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| स्वरूप: | लेख |
| भाषा: | English |
| प्रकाशित: |
Isfahan University of Technology
2021-01-01
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| श्रृंखला: | Journal of Applied Fluid Mechanics |
| विषय: | |
| ऑनलाइन पहुंच: | http://jafmonline.net/JournalArchive/download?file_ID=54982&issue_ID=1011 |