Effects of stator splitter blades on aerodynamic performance of a single-stage transonic axial compressor
Splitter blades located between stator blades in a single-stage axial compressor were proposed and investigated in this work to find their effects on aerodynamic performance and operating stability. Aerodynamic performance of the compressor was evaluated using three-dimensional Reynolds-averaged Na...
محفوظ في:
| المؤلفون الرئيسيون: | , , |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
Universiti Malaysia Pahang Al-Sultang Abdullah Publishing
2020-12-01
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| سلاسل: | Journal of Mechanical Engineering and Sciences |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://journal.ump.edu.my/jmes/article/view/3358 |
| الوسوم: |
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