2020
DOI: 10.1007/978-3-030-58362-0_23
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Total Fatigue Life Estimation of Aircraft Structural Components Under General Load Spectra

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“…After gathering the data, a filtration must be applied to properly represent loads that could be reenacted on the analyzed structure by means of an experiment (Rodzewicz & Przekop, 2000) or a simulation (Maksimovic et al, 2021). In aircrafts, while some events and resulting accelerations may be treated as random (mainly gusts and landings), flight loads can be assumed as mostly deterministic ("Load Spectra", 2009).…”
Section: Introductionmentioning
confidence: 99%
“…After gathering the data, a filtration must be applied to properly represent loads that could be reenacted on the analyzed structure by means of an experiment (Rodzewicz & Przekop, 2000) or a simulation (Maksimovic et al, 2021). In aircrafts, while some events and resulting accelerations may be treated as random (mainly gusts and landings), flight loads can be assumed as mostly deterministic ("Load Spectra", 2009).…”
Section: Introductionmentioning
confidence: 99%