Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count
This study investigates the aerodynamic and aeroelastic characteristics of a transonic axial compressor, focusing on blade count reduced rotor behavior. The analysis is based on experiments, conducted at the Transonic Compressor Darmstadt test rig at Technical University of Darmstadt and compulsory...
محفوظ في:
| المؤلفون الرئيسيون: | , , , , , |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
MDPI AG
2021-06-01
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| سلاسل: | International Journal of Turbomachinery, Propulsion and Power |
| الموضوعات: | |
| الوصول للمادة أونلاين: | https://www.mdpi.com/2504-186X/6/2/19 |
| الوسوم: |
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