Fatigue Life of a Structurally Like Sample of a Fuselage Panel with an Aluminum–Glass-Reinforced Plastic Shell

Autor:	Yu. M. Stoida, V. V. Sidel’nikov, T. S. Rodchenko, M. D. Zaitsev, V. V. Antipov, N. Yu. Serebrennikova
Rok vydání:	2021
Předmět:	Materials science Tension (physics) Alloy Metals and Alloys Shell (structure) chemistry.chemical_element Fibre-reinforced plastic engineering.material Cracking Fuselage chemistry Aluminium engineering Composite material GLARE
Zdroj:	Russian Metallurgy (Metally). 2021:400-405
ISSN:	1555-6255 0036-0295
DOI:	10.1134/s0036029521040030
Popis:	Comparative tests are performed during repeated tension of structurally similar samples of fuselage panels with a SIAL-3-1R laminated aluminum–glass-reinforced plastic (GRP) shell and a shell made of aluminum alloy 1163 sheets, and their fatigue life until cracking and complete failure is determined. Instrumental methods of monitoring the integrity of the structure with the registration of cracks up to 5 mm long and monitoring their growth have been tested. Fractographic studies of the crack development of in the layered aluminum–GRP material are carried out. The advantages of using a metal–polymer layered material as the shell of aircraft fuselage panels in comparison with a traditional aluminum alloy are shown.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::9605da0b7cba8e17ffa5361d10d94ce2 https://doi.org/10.1134/s0036029521040030 Zobrazit plný text záznamu Full text from SpringerLink