NDLI: Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites. phase 3: major component development

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Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites. phase 3: major component development

Content Provider	NASA Technical Reports Server (NTRS)
Author	Bryson, L. L. McCarty, J. E.
Copyright Year	1973
Description	Analytical and experimental investigations, performed to establish the feasibility of reinforcing metal aircraft structures with advanced filamentary composites, are reported. Aluminum-boron-epoxy and titanium-boron-epoxy were used in the design and manufacture of three major structural components. The components were representative of subsonic aircraft fuselage and window belt panels and supersonic aircraft compression panels. Both unidirectional and multidirectional reinforcement concepts were employed. Blade penetration, axial compression, and inplane shear tests were conducted. Composite reinforced structural components designed to realistic airframe structural criteria demonstrated the potential for significant weight savings while maintaining strength, stability, and damage containment properties of all metal components designed to meet the same criteria.
File Size	41252392
Page Count	113
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19740006512
Archival Resource Key	ark:/13960/t8dg1hk0r
Language	English
Publisher Date	1973-11-01
Access Restriction	Open
Subject Keyword	Structural Mechanics Boron Composite Materials Reinforcement Structures Aluminum Epoxy Resins Mechanical Properties Titanium Aircraft Structures 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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