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- W2383265312 abstract "The cracks at the joint bolt for the wing and fuselage of an aircraft were observed,when the aircraft was experienced a field maintenance,as a result of analyzing the relevant macroscopic and microscopic features of the fracture,measuring the change of chemical compositions around cracks,as well as combining the repairing process for bolts,the reason for the cracks generation was found out." @default.
- W2383265312 created "2016-06-24" @default.
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- W2383265312 date "2005-01-01" @default.
- W2383265312 modified "2023-09-24" @default.
- W2383265312 title "ANALYSIS OF CRACKING OF JOINT BOLT FOR WING AND FUSELAGE OF AN AIRCRAFT" @default.
- W2383265312 hasPublicationYear "2005" @default.
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