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Miscellanea Views: 884 Downloads: 651 Vol. 5, No. 16 (2011) pp. pages 34-42

Damage tolerance analysis of aircraft reinforced panels

F. Carta, A. Pirondi

This work is aimed at reproducing numerically a campaign of experimental tests performed for the development of reinforced panels, typically found in aircraft fuselage. The bonded reinforcements can significantly reduce the rate of fatigue…

10.3221/IGF-ESIS.16.04

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Failure Analysis, Case Studies and Forensic Engineering Views: 596 Downloads: 716 Vol. 15, No. 58 (2021) September 25, 2021 pp. 211-230

A new methodology to predict damage tolerance based on compliance via global-local analysis

Gilberto Gomes, Thiago Oliveira, Alvaro Martins

Over the years several design philosophies to fatigue developed in order to combine structural safety and economy to manufacturing and operating aircraft process. The safe-life approach, which consists of designing and manufacturing a safe…

10.3221/IGF-ESIS.58.16

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SI: Portuguese contributions for Structural Integrity Views: 1,513 Downloads: 701 Vol. 13, No. 48 (2019) March 5, 2019 pp. 269-285

Development of hybrid friction stir welding and adhesive bonding single lap joints in aluminium alloys

Ricardo Leite Maciel, Virginia Infante, Daniel Braga, Pedro Moreira, Tiago Bento, Lucas da Silva

Aircraft have been manufactured for decades using a wide variety of welding and joining techniques. There have been signiﬁcant developments in techniques over the last 15–20 years. In civil aeronautical industry the main materials used for…

10.3221/IGF-ESIS.48.28

Details: Development of hybrid friction stir welding and adhesive bonding single lap joints in aluminium alloys PDF Visual Abstract

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Damage tolerance analysis of aircraft reinforced panels

A new methodology to predict damage tolerance based on compliance via global-local analysis

Development of hybrid friction stir welding and adhesive bonding single lap joints in aluminium alloys