Accession Number : ADA305101
Title : Carbon Fibre Study Number 4, Failure Criteria of CFRP Composites at Cryogenic Temperatures.
Descriptive Note : Technical rept.,
Corporate Author : BRITISH AEROSPACE PLC HATFIELD (UNITED KINGDOM) AIR WEAPONS DIV
Personal Author(s) : Rickett, M. F.
PDF Url : ADA305101
Report Date : MAY 1978
Pagination or Media Count : 196
Abstract : Test performed during the Spacelab Support Research and Technology Programme involving a Carbon Fibre Reinforced Plastic faced honeycomb panel have been rerun using an improved experimental technique. The original theoretical analysis has been revised using CFRP material parameters derived from a separate coupon test programme. Results from this programme have shown only small changes in material properties with decreasing temperatures. Discrepancies that were found between theoretical and practical panel performance have been put down to anomalous expansion coefficients and detail model problems. (AN)
Descriptors : *FIBER REINFORCED COMPOSITES, *REINFORCED PLASTICS, STRESS STRAIN RELATIONS, MATHEMATICAL MODELS, LOAD DISTRIBUTION, LOW TEMPERATURE, TENSILE STRENGTH, STRESS ANALYSIS, LAMINATES, FINITE ELEMENT ANALYSIS, STRUCTURAL ANALYSIS, TENSILE STRESS, SHEAR MODULUS, STIFFNESS, CRACKING(FRACTURING), CARBON FIBERS, TEMPERATURE GRADIENTS, ALUMINUM, THERMAL EXPANSION, FLEXURAL STRENGTH, STRAIN GAGES, CREEP, FAILURE(MECHANICS), COMPRESSIVE STRENGTH, CRYOGENICS, THERMAL CYCLING TESTS, BENDING STRESS, SANDWICH PANELS, SHEAR STRENGTH, HONEYCOMB STRUCTURES.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE