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- W1548444629 abstract "Aluminum honeycomb sandwich structures are known to have not only a high flexural rigidity and strength with a relatively low density ratio but also excellence in anti-vibration and anti-noise properties. These characteristics are essential in the design of airplanes and high-speed ships that require light and high strength. In this paper, the Reissner-Mindlin shear deformation and rotary inertia plate theory was introduced to the rectangular sandwich plate expanded from Hamilton’s principle. The results from the equation of motion based on Hamilton’s principle were compared with those from the Rayleigh-Ritz method. The applied sandwich models consisted of isotropic and symmetrical aluminum and aluminum honeycomb cores. The structures used for the study had 4 plates with various thicknesses and cores of different cell sizes. This kind of structure was used for a seawater survey ship (SWSS) in Japan in 1993 (Paik and Lee, 1995; Kaneko, Takeuchi and Aokage, 1993). The boundary conditions considered in the research were simple, fixed and free supports. Received March 19, 1997: revised manuscript received by the editors January 19, 1998. The original version (prior to the final revised manuscript) was presented at the Seventh International Offshore and Polar Engineering Conference (ISOPE-97), Honolulu, USA, May 2530, 1997." @default.
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- W1548444629 date "1998-06-01" @default.
- W1548444629 modified "2023-09-23" @default.
- W1548444629 title "An Experimental Study On the Structural Behavior And Vibrational Characteristics of Sandwich Plate With Aluminium Honeycomb Core" @default.
- W1548444629 hasPublicationYear "1998" @default.
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