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- W3012735331 abstract "Aircraft structures consist of largely thin sheets stiffened by different shape of stringers. If damage occurs to the thin sheet, a normal procedure taken is to remove the damage area usually in the shape of rectangular hole which is rounded at the corners to reduce the stress concentration. The area is then reinforced with a repair patch riveted to the sheet. Riveted joint is one of the most methods that are usually used by aircraft manufacturer to repair an aircraft structure. The important thing in analysis of riveted joint is to compute the transfer of load in each of rivet. In this project, the analysis of riveted joint is using finite element method and the stiffness of rivet is calculated by using Vlieger/Broek method." @default.
- W3012735331 created "2020-03-27" @default.
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- W3012735331 date "2020-01-16" @default.
- W3012735331 modified "2023-09-26" @default.
- W3012735331 title "ANALYSIS OF RIVETED JOINT USING VLIEGER/BROEK EQUATION" @default.
- W3012735331 hasPublicationYear "2020" @default.
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