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Analysis of Thick Sandwich Shells with Embedded Ceramic TilesThe Composite Armored Vehicle (CAV) is an advanced technology demonstrator of an all-composite ground combat vehicle. The CAV upper hull is made of a tough light-weight S2-glass/epoxy laminate with embedded ceramic tiles that serve as armor. The tiles are bonded to a rubber mat with a carefully selected, highly viscoelastic adhesive. The integration of armor and structure offers an efficient combination of ballistic protection and structural performance. The analysis of this anisotropic construction, with its inherent discontinuous and periodic nature, however, poses several challenges. The present paper describes a shell-based 'element-layering' technique that properly accounts for these effects and for the concentrated transverse shear flexibility in the rubber mat. One of the most important advantages of the element-layering technique over advanced higher-order elements is that it is based on conventional elements. This advantage allows the models to be portable to other structural analysis codes, a prerequisite in a program that involves the computational facilities of several manufacturers and government laboratories. The element-layering technique was implemented into an auto-layering program that automatically transforms a conventional shell model into a multi-layered model. The effects of tile layer homogenization, tile placement patterns, and tile gap size on the analysis results are described.
Document ID
19970003306
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Davila, Carlos G.
(Army Research Lab. Hampton, VA United States)
Smith, C.
(United Defense, Ltd. Partnership San Jose, CA United States)
Lumban-Tobing, F.
(United Defense, Ltd. Partnership San Jose, CA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:110278
ARL-TR-1213
NASA-TM-110278
Report Number: NAS 1.15:110278
Report Number: ARL-TR-1213
Report Number: NASA-TM-110278
Meeting Information
Meeting: Conference on Fibrous Composites in Structural Design
Location: Fort Worth, TX
Country: United States
Start Date: August 26, 1996
End Date: August 30, 1996
Sponsors: NASA Langley Research Center, Federal Aviation Administration, Department of Defense
Accession Number
97N12050
Funding Number(s)
PROJECT: RTOP 505-63-50-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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