Accession Number : ADA308518
Title : Mechanical Behavior of Boron-Epoxy and Glass-Epoxy Filament-Wound Cylinders Under Various Loads.
Descriptive Note : Technical note,
Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER
Personal Author(s) : Herring, Harvey W. ; Baucom, Robert M. ; Pride, Richard A.
PDF Url : ADA308518
Report Date : MAR 1969
Pagination or Media Count : 69
Abstract : A study was made to determine the mechanical behavior of boron-epoxy and S-glass-epoxy filament-wound cylinders under tensile, compressive, torsional, and pressure loads. These cylinders were fabricated in either an orthotropic winding pattern or an isotropic pattern. Conventional theory used to predict the elastic behavior of glass-epoxy filament-wound cylinders was discovered to be equally adequate for the boron-epoxy cylinders. Attempts to correlate cylinder failure strengths calculated from existing state-of-the-art theories with experimental failure strengths met with varying success.
Descriptors : *EPOXY COMPOSITES, *PLASTICS, *GLASS REINFORCED PLASTICS, LOAD DISTRIBUTION, FILAMENT WOUND CONSTRUCTION, FIBER REINFORCED COMPOSITES, ELASTIC PROPERTIES, MODULUS OF ELASTICITY, STRAIN(MECHANICS), CYLINDRICAL BODIES, SHEAR STRESSES, BUCKLING, BORON, FAILURE(MECHANICS), COMPRESSIVE STRENGTH, POLYESTER PLASTICS, POISSON RATIO, INTERNAL PRESSURE, PHOTOMICROGRAPHY.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE