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- W2321814368 abstract "A sandwich panel is a composite structure consisting of two thin and stiff face sheets bonded to a thick and low weight core. Sandwich structures offer great potential for the development of optimized structures with high stiffness and strength-to-weight ratios. Sandwich structures are found in ground transportation, aircraft, naval and aerospace structures where low weight is required. A major concern when using such materials is the bonding between the face sheets and core. Adequate bonding is necessary to warrant load transfer between the face sheets in order to utilize the full potential that a sandwich structure offers. Face-to-core debonds might arise as a consequence of improper manufacturing procedures, or in-service loads such as hard object impact loading or blast situations. A face/core debond degrades the structural integrity of the sandwich and may led to premature failure, especially when the sandwich is loaded in compression. Under in-plane compressive loading, the face sheet over the debond might buckle and grow triggering structural collapse. The compressive failure mechanism of sandwich specimens containing impact damage or artificially created face/core debonds has been the subject of several research papers published in recent years. This chapter reviews experimental studies of the failure mechanisms of debonded sandwich columns and panels loaded in compression and examines the in-plane and out-of-plane compressive loading." @default.
- W2321814368 created "2016-06-24" @default.
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- W2321814368 date "2008-01-01" @default.
- W2321814368 modified "2023-09-23" @default.
- W2321814368 title "Experimental studies of compression failure of sandwich specimens with face/core debond" @default.
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- W2321814368 doi "https://doi.org/10.1533/9781845694821.3.344" @default.
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