Design and analysis of aeronautical repair: fastened x bonded (2010)
- Authors:
- Autor USP: TITA, VOLNEI - EESC
- Unidade: EESC
- Subjects: MÉTODO DOS ELEMENTOS FINITOS; FADIGA DE AERONAVES; AERONAVES; ENGENHARIA AERONÁUTICA
- Language: Inglês
- Imprenta:
- Publisher: SAE Brasil
- Publisher place: São Paulo, SP
- Date published: 2010
- Source:
- Título: Proceedings
- Conference titles: Congresso e Exposição Internacionais de Tecnologia da Mobilidade
-
ABNT
RIBEIRO, Marcelo Leite et al. Design and analysis of aeronautical repair: fastened x bonded. 2010, Anais.. São Paulo, SP: SAE Brasil, 2010. Disponível em: https://repositorio.usp.br/directbitstream/e1893c8e-303b-4c1f-bf2a-3a63ce4848d2/trabalho%20117%20-%20Design%20and%20analysis%20of%20aeronautical%20repair%20fastened%20x%20bonded.%20%28Congresso%20SAE%20BRASIL%202010%29_removed.pdf. Acesso em: 23 jan. 2026. -
APA
Ribeiro, M. L., Barbosa, A. A. F., Di Salvo, F., Borges, E. N., Basile, T. F., & Tita, V. (2010). Design and analysis of aeronautical repair: fastened x bonded. In Proceedings. São Paulo, SP: SAE Brasil. Recuperado de https://repositorio.usp.br/directbitstream/e1893c8e-303b-4c1f-bf2a-3a63ce4848d2/trabalho%20117%20-%20Design%20and%20analysis%20of%20aeronautical%20repair%20fastened%20x%20bonded.%20%28Congresso%20SAE%20BRASIL%202010%29_removed.pdf -
NLM
Ribeiro ML, Barbosa AAF, Di Salvo F, Borges EN, Basile TF, Tita V. Design and analysis of aeronautical repair: fastened x bonded [Internet]. Proceedings. 2010 ;[citado 2026 jan. 23 ] Available from: https://repositorio.usp.br/directbitstream/e1893c8e-303b-4c1f-bf2a-3a63ce4848d2/trabalho%20117%20-%20Design%20and%20analysis%20of%20aeronautical%20repair%20fastened%20x%20bonded.%20%28Congresso%20SAE%20BRASIL%202010%29_removed.pdf -
Vancouver
Ribeiro ML, Barbosa AAF, Di Salvo F, Borges EN, Basile TF, Tita V. Design and analysis of aeronautical repair: fastened x bonded [Internet]. Proceedings. 2010 ;[citado 2026 jan. 23 ] Available from: https://repositorio.usp.br/directbitstream/e1893c8e-303b-4c1f-bf2a-3a63ce4848d2/trabalho%20117%20-%20Design%20and%20analysis%20of%20aeronautical%20repair%20fastened%20x%20bonded.%20%28Congresso%20SAE%20BRASIL%202010%29_removed.pdf - A new SHM methodology applied on composite plates
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