Go to:
Logótipo
You are in:: Start > Publications > View > Multi-Site Damage in riveted lap joints: experimental simulation and finite element prediction
Map of Premises
FC6 - Departamento de Ciência de Computadores FC5 - Edifício Central FC4 - Departamento de Biologia FC3 - Departamento de Física e Astronomia e Departamento GAOT FC2 - Departamento de Química e Bioquímica FC1 - Departamento de Matemática
Publication

Multi-Site Damage in riveted lap joints: experimental simulation and finite element prediction

Title
Multi-Site Damage in riveted lap joints: experimental simulation and finite element prediction
Type
Thesis
Year
1999
Authors
Lucas Filipe Silva
(Author)
FEUP
View Personal Page You do not have permissions to view the institutional email. Search for Participant Publications View Authenticus page Without ORCID
Scientific classification
FOS: Engineering and technology > Other engineering and technologies
CORDIS: Technological sciences > Engineering > Aerospace engineering
Other information
Resumo (PT): Desde o acidente do avião da companhia Aloha em 1988, o problema do ‘Multiple Site Damage’ (MSD) de juntas de sobreposição rebitadas de fuselagens de aviões tem recebido muita atenção. O custo de novos aviões implica a existência neste momento de frotas antigas requerendo uma análise especial. A investigação no campo das estruturas contendo MSD tem recebido grande atenção internacional. O objectivo deste estudo é gerar dados sobre a iniciação e o crescimento de fendas, e a resistência residual de provetes de laboratório que simulam as principais características de juntas de aviões contendo MSD. Estes dados serão usados para avaliar um modelo baseado no FRANC2D/L, programa de elementos finitos.
Abstract (EN): Since the Aloha accident in 1988, the Multiple Site Damage (MSD) problem of riveted lap joints in aircraft fuselages has drawn much attention. The cost of new aircraft implies that there are now ageing fleets requiring special analysis. There is a need for research into the field of structures containing MSD, topic which has recently received world-wide attention. The objective of the present study is to generate data on the initiation and growth of cracks, and on the residual static strength of laboratory specimens which simulate the key features of aircraft joints in which MSD is present. These data will be used to assess the predictive model based in the FRANC2D/L finite element programme.
Language: Portuguese
Type (Professor's evaluation): Scientific
No. of pages: 190
Documents
We could not find any documents associated to the publication.
Related Publications

Of the same authors

Adhesive joints for low and high temperatures (2004)
Thesis
Lucas Filipe Martins da Silva; R.D. Adams; Sem Nome; R.D.Adams
Introdução às ligações adesivas estruturais (2021)
Educational Publication
da Silva, LFM; Marques, EAS; Ricardo Carbas; Francisco Tenreiro
Adhesive Bonding Technology and Testing (2023)
Educational Publication
da Silva, LFM; Marques, EAS; Ricardo Carbas; Alireza Akhavan-Safar
Torsion machine for adhesive joints (2016)
Patent
da Silva, LFM; André Guimarães; J A Gonçalves; Ricardo Carbas; António Mendes Lopes; Carlos Moreira da Silva

See all (636)

Of the same scientific areas

Three-dimensional stress intensity factor calibration for a stiffened cracked plate (2009)
Article in International Scientific Journal
P. M. G. P. Moreira; S. D. Pastrama; P. M. S. T. de Castro
Tailoring for strength of composite steered-fibre panels with cutouts (2010)
Article in International Scientific Journal
Lopes, CS; Gurdal, Z; Camanho, PP
Hybrid titanium-CFRP laminates for high-performance bolted joints (2009)
Article in International Scientific Journal
Camanho, PP; Fink, A; Obst, A; Pimenta, S
Fatigue striation spacing size in Al 2024-T3 and equivalent initial flaw riveted specimens (2005)
Article in International Scientific Journal
Pedro Moreira; Paulo Matos; Paulo Tavares De Castro
Recommend this page Top
Copyright 1996-2024 © Faculdade de Ciências da Universidade do Porto  I Terms and Conditions  I Acessibility  I Index A-Z  I Guest Book
Page created on: 2024-07-23 at 03:32:40 | Acceptable Use Policy | Data Protection Policy | Complaint Portal