Multiaxial fatigue of in-service aluminium longerons for helicopter rotor-blades

Fatigue cracking of longerons manufactured from Al-alloy AVT-1 for helicopter in-service rotor-blades was considered and crack growth period and equivalent of tensile stress for different blade sections were estimated. Complicated case of in-service blades multiaxial cyclically bending-rotating and...

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Bibliographic Details
Main Authors: A. Shanyavskiy, A. Toushentsov
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2016-10-01
Series:Frattura ed Integrità Strutturale
Subjects:
Online Access:http://www.gruppofrattura.it/pdf/rivista/numero38/numero_38_art_49.pdf