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- W2207284613 abstract "The application of crack growth predictions in aeronautics has been highly stimulated by airworthiness requirements imposed by government and military agencies. These requirements were initiated to ensure the fatigue safety and durability of a fleet of aircraft. Small cracks either pre-existing at the time of manufacture or created by in-service conditions are assumed to grow during the life of the aircraft. The growth of the crack should be predictable to provide guidance for inspection program, which ensure that cracks will never propagate to failure prior to detection. The ONERA model was proposed by Baudin and Robert from ONERA, France. They assume that the crack opening load is limited by two extreme conditions i.e. the constant-amplitude case and the single overload case. For variable-amplitude, the crack opening level is between these two cases, depending on a load spectrum parameter. The model includes considerations on plane stress and plane strain conditions and the effect of material thickness. The evaluation of the model is intended to explore the mechanism of the model and to analyse the predicted results by comparing to some test result data. Effect of some parameters in aircraft spectrum loading are examined. Some conclusions are drawn related to superiorities and shortcomings of the model." @default.
- W2207284613 created "2016-06-24" @default.
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- W2207284613 date "1996-01-01" @default.
- W2207284613 modified "2023-09-24" @default.
- W2207284613 title "Evaluation of the ONERA Model in Predicting Fatigue Crack Growth under Aircraft Spectrum Loading" @default.
- W2207284613 hasPublicationYear "1996" @default.
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