Stress state analysis of compressor blade-disk joint with the influence of centrifugal forces and blade mistuning

The authors present the results of the numerical experiments on the determination of the effect of compressor blade mistuning on the stress state of a blade-disk joint under the action of the centrifugal forces and their comparison with results of full-scale experiments. The analysis of the results...

Descripción completa

Guardado en:
Detalles Bibliográficos
Autores principales: Анатолій Павлович Зіньковський, Вячеслав Михайлович Меркулов, Олег Леонідович Деркач, Іван Гордійович Токар, Кирило Валентинович Савченко
Formato: article
Lenguaje:EN
RU
UK
Publicado: National Aerospace University «Kharkiv Aviation Institute» 2021
Materias:
Acceso en línea:https://doaj.org/article/b7b9c9aa612441ec8fab10208857d69d
Etiquetas: Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!