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- W2009125655 abstract "This paper describes the development of damped structure for the Supportable Technology for Affordable Fighter Structures (STAFS) Program. The study started with analytical design trade studies and progressed through a series of tests to characterize adhesive behavior, performance testing of a component level integrally damped panel concept, and full scale design integration. Analyses were performed on finite element panel models with viscoelastic elements in the bond areas to determine the sensitivities of configuration and adhesive type to overall damping achieved. The concepts studied showed that as much as 10 percent structural damping could be obtained in the structural modes of interest. Test panels with and without damping treatments were fabricated using super plastically formed-adhesive bonded 2095 aluminum, and tested to measure the comparative response improvement in the damped panels. A substantial weight savings was realized in comparison to the monolithic metal panels which would be required to withstand the acoustic environment.© (1995) COPYRIGHT SPIE--The International Society for Optical Engineering. Downloading of the abstract is permitted for personal use only." @default.
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- W2009125655 date "1995-05-05" @default.
- W2009125655 modified "2023-09-23" @default.
- W2009125655 title "<title>Integral passive damping for aircraft fuselage structure</title>" @default.
- W2009125655 doi "https://doi.org/10.1117/12.208909" @default.
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