Fatigue Crack Growth Simulation
Mostrando 1-4 de 4 artigos, teses e dissertações.
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1. Experimental Study of Fatigue Crack Behavior of Rib-To-Rib Butt Welded Connections in Orthotropic Steel Decks
Abstract Rib-to-rib (RR) butt welded connections are one of the most sensitive locations for encountering fatigue failure in orthotropic steel decks (OSDs), and numerous fatigue cracks arising from these areas have been identified in existing OSD bridges. Due to dynamic factors in their service life bridges with an orthotropic steel deck (OSD) are prone to f
Lat. Am. j. solids struct.. Publicado em: 11/10/2018
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2. Avaliação da propagação de trinca associada à corrosão da liga 7475 T7351 submetida a carregamentos de voos simulados / Evaluation of corrosion fatigue crack growth for 7475 T7351 alloy under spectrum loading
A análise da vida em fadiga em amplitude variável associada à corrosão é bastante complexa, devido a combinações entre as interações eletroquímicas ocorridas, tendo em vista a exposição da frente da trinca à névoa salina somada aos efeitos deletérios do carregamento de amplitude variável. Esta combinação de efeitos ainda não é modelada ma
IBICT - Instituto Brasileiro de Informação em Ciência e Tecnologia. Publicado em: 13/07/2012
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3. Sobre metodologias de modelagem computacional de propagação de trincas por fadiga em fuselagens aeronáuticas. / On computacional modeling methodologies of fatigue crack propagation in aircraft fuselages.
A methodology for modeling fatigue crack growth in pressurized, stiffened, thin shell structures is implemented within a software framework that consists of a fracture simulation code associated with a finite element analysis code. Crack trajetories are allowed to be arbitrary and are computed incrementally as a part of the simulation. Trajectories are repre
Publicado em: 2007
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4. Sobre a modelagem da propagação de trincas por fadiga em estruturas de cascas pressurizadas. / On the modeling of fatigue crack propagation in pressurized shell structures.
The modeling of fatigue crack growth in pressurized fuselages is very complex due to many factors, such as the nonlinear stiffening effect referred to as bulging, the fuselage skin being very thin and the presence of stiffeners which modifies the stress distribution on the fuselage. A methodology for the computational modeling of the fatigue crack growth in
Publicado em: 2006