Accession Number : AD0732489
Title : Determination of Physical and Structural Properties of Mixed-Modulus Composite Materials
Descriptive Note : Final rept.
Corporate Author : BOEING VERTOL CO PHILADELPHIA PA
Personal Author(s) : Pinckney, Robert L ; Freeman, Richard B
PDF Url : AD0732489
Report Date : Jun 1971
Pagination or Media Count : 70
Abstract : The objective of this program was to determine the physical and structuralproperties of mixed-modulus composite materials using combinations of graphiteand S-glass fibers with epoxy resin under static and fatigue loading conditions.The data obtained for solid laminates, tubular specimens and sandwich beamsin which the S-glass material was oriented parallel to the longitudinal axisof the specimens and the graphite fibers were oriented at plus or minus 45to the same axis, are reported. Stress-strain and S-N CURVES ARE COMPARED TOAPPROPRIATE DATA ON PURE S-glass and pure graphite material where such datacontributes to an understanding of the mixed materials performance. The dataindicates that the mixed-modulus system is compatible with the structural andfailure mode requirements of helicopter rotor blades.
Descriptors : *COMPOSITE MATERIALS, *REINFORCING MATERIALS, ALIGNMENT, CARBON FIBERS, CREEP, FAILURE(MECHANICS), FATIGUE(MECHANICS), GLASS TEXTILES, HELICOPTER ROTORS, LAMINATES, MODULUS OF ELASTICITY, PHYSICAL PROPERTIES, PIPES, ROTOR BLADES(ROTARY WINGS), SANDWICH CONSTRUCTION
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE