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