Fatigue damage in aircraft structures, not wanted, but tolerated?

DOI10.1016/J.IJFATIGUE.2008.05.016zbMath1419.74023OpenAlexW1982783541MaRDI QIDQ1016267

Jaap Schijve

Publication date: 5 May 2009

Published in: International Journal of Fatigue (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijfatigue.2008.05.016

zbMATH Keywords

damage toleranceaircraft structurescase historiesdesign against fatiguerealistic testing

Mathematics Subject Classification ID

Experimental work for problems pertaining to mechanics of deformable solids (74-05) Fracture and damage (74R99)

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Damage identification in aluminum plates based on iterative partition algorithm using waveform centroid ⋮ Mooring system design optimization using a surrogate assisted multi-objective genetic algorithm ⋮ Multiscale aircraft fuselage fatigue analysis by the dual boundary element method ⋮ Productivity with fatigue and long memory: fractional calculus approach ⋮ Fatigue effects in elastic materials with variational damage models: a vanishing viscosity approach ⋮ Asymptotic decomposition in the problem of joined elastic plates ⋮ A general phase-field model for fatigue failure in brittle and ductile solids

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