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- W2293942533 abstract "In order to illustrate the failure mechanism of multi-site-damage (MSD) in aging aircraft structures, multiple crack growth tests of simulated aircraft fuselage skin panels were conducted. Since local buckling near rivets affects crack growth, the panels were loaded in two different cases. The first is a buckling-free case where the panel is not restrained from out-of-plane buckling. In the other case, buckling is restrained by a buckle restraining cover plate. The emphasis of this paper is on the establishment of crack growth mechanisms in an aircraft fuselage based on the experimental results. With the aid of holographic interferometry, the factors controlling the formation and the growth of cracks under the above loading conditions are investigated and discussed." @default.
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- W2293942533 date "1995-01-01" @default.
- W2293942533 modified "2023-09-22" @default.
- W2293942533 title "Crack Growth Modelling and Experiment in Airframes" @default.
- W2293942533 hasPublicationYear "1995" @default.
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