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- W1978837586 abstract "Composite sandwich panels are increasingly attractive structural components for modern space structures. Their light weight, high stiffness, and 'manufacturability' make them ideal for primary structure. One disadvantage of sandwich panels is the low damping, typically on the order of 0.5 percent. This problem has been addressed during the course of designing an all composite spacecraft bus. A visco-elastic treatment and a constraining layer have been applied to a composite sandwich panel. Analysis and tests were performed on the panel in both the damped, and the un-damped configuration. A five-fold increase in the panel damping was achieved, and some valuable lessons learned. These lessons, the modeling methods, test and analysis results are presented." @default.
- W1978837586 created "2016-06-24" @default.
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- W1978837586 date "1996-05-01" @default.
- W1978837586 modified "2023-09-23" @default.
- W1978837586 title "<title>Analysis and test of a damped composite sandwich structure</title>" @default.
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- W1978837586 doi "https://doi.org/10.1117/12.239100" @default.
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