NDLI: Boron/aluminum-graphite/resin advanced fiber composite hybrids

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Boron/aluminum-graphite/resin advanced fiber composite hybrids

Content Provider	NASA Technical Reports Server (NTRS)
Author	Sullivan, T. L. Lark, R. F. Chamis, C. C.
Copyright Year	1974
Description	An investigation was conducted to determine the fabrication feasibility and to assess the potential of adhesively-bonded metal and resin matrix fiber composite hybrids as an advanced material, for aerospace and other structural applications. The results of fabrication studies and of evaluation of physical and mechanical properties show that using this hybrid concept it is possible to design a composite which, when compared to nonhybrid composites, has improved transverse strength, transverse stiffness, and impact resistance with only a small penalty on density and longitudinal properties. The results also show that laminate theory is suitable for perdicting the structural response of such hybrids. The sequence of fracture modes indicates that these types of hybrids can be readily designed to meet fail-safe requirements.
File Size	1914245
Page Count	19
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19740021889
Archival Resource Key	ark:/13960/t4pk5591f
Language	English
Publisher Date	1974-01-01
Access Restriction	Open
Subject Keyword	Materials, Nonmetallic Stresses Boron Composite Materials Aluminum Graphite Impact Resistance Feasibility Analysis Adhesive Bonding Laminates Fibers Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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