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...
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| Format: | Article |
| Language: | English |
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University of West Bohemia
2017-06-01
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| Series: | Applied and Computational Mechanics |
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| Online Access: | https://www.kme.zcu.cz/acm/acm/article/view/324/406 |