Simulation of dynamic impact of an aircraft engine on aircraft wing caused by a fan blade breakaway
One of the requirements for a projected aircraft is the ability to continue flying and land in the event of a breakdown of one of the engines. One of the calculated cases of engine breakdown is a fan blade breakaway. This phenomenon causes large vibrations of both the engine itself and the aircraft...
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| Formato: | article |
| Lenguaje: | EN RU UK |
| Publicado: |
National Aerospace University «Kharkiv Aviation Institute»
2021
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| Materias: | |
| Acceso en línea: | https://doaj.org/article/e833827759644f00b721077d7f64c28a |
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