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The bending behavior of a curved sandwich panel with a transversely flexible core, i.e., "soft" in the out of plane direction is derived. It is formulated using a rigorous systematic closed-form approach based on variational principles. The effects of the transversely flexible core are...
This paper presents a preliminary study of sound transmission loss of sandwich aircraft structures for global transportation applications. A review of the literature on the related research is given. Some research issues are identified that are important to reducing interior noise of aircraft....
A new test specimen, denoted "Tilted Sandwich Debond" (TSD) specimen, for characterization of debond failure of foam core sandwich structure is experimentally examined. The bottom face of a sandwich is attached to an incline, and debond progression is examined under vertical load application to...
The results of detailed study of the effect of the cutout on the response of curved sandwich panels are presented. The panels have honeycomb core composite face sheets. The loading consists of a temperature gradient through-the-thickness combined with pressure loading and edge shortening or edge...
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