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- W2393854655 abstract "The failure analysis of crack on a certain type of aircraft's strengthened wing rib components were accomplished based on chemical composition analysis,metallographic examination,hardness testing,fracture morphology analysis and performance analysis.The results show that the manufacturing quality of the strengthened wing rib component is normal without defect.Low cycle fatigue fracture on the strengthened wing rib components appears because the structural design is undeserved and it causes too big impact load stress." @default.
- W2393854655 created "2016-06-24" @default.
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- W2393854655 date "2013-01-01" @default.
- W2393854655 modified "2023-09-28" @default.
- W2393854655 title "Failure Analysis of Crack on Aircraft's Strengthened Wing Rib Component" @default.
- W2393854655 hasPublicationYear "2013" @default.
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