Whirl flutter optimisation-based solution of twin turboprop aircraft using a full-span model
Whirl flutter is a specific type of flutter instability, relevant for turboprop aircraft, caused by the effect of rotating parts as a propeller or a gas-turbine engine rotor. The proposed optimisation-based analytical procedure is used to determine the critical values of the engine attachment stiffn...
محفوظ في:
| المؤلف الرئيسي: | |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
University of West Bohemia in Pilsen
2017-06-01
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| سلاسل: | Applied and Computational Mechanics |
| الموضوعات: | |
| الوصول للمادة أونلاين: | https://www.kme.zcu.cz/acm/acm/article/view/324/406 |
| الوسوم: |
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