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Volumn 19, Issue 1, 1998, Pages 65-70
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The gradient of mechanical characteristics across the thickness of composite laminates after exposure to a low earth orbit environment
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Author keywords
[No Author keywords available]
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Indexed keywords
AIRCRAFT MATERIALS;
CARBON FIBER REINFORCED PLASTICS;
ELASTIC MODULI;
EPOXY RESINS;
GLASS FIBER REINFORCED PLASTICS;
GLASS TRANSITION;
LAMINATED COMPOSITES;
MICROHARDNESS;
SPACECRAFT;
THERMAL CYCLING;
THERMAL EXPANSION;
COMMUNICATION SATELLITES;
DILATOMETERS;
DYNAMIC MECHANICAL ANALYSIS;
DYNAMICS;
ELASTOMERS;
FIBER REINFORCED PLASTICS;
GLASS;
LAMINATES;
MECHANICAL PROPERTIES;
ORBITS;
DYNAMIC MECHANICAL ANALYSIS (DMA);
DYNAMIC SHEAR MODULUS;
LINEAR DILATOMETRY (LD);
THERMAL EXPANSION COEFFICIENT;
PLASTIC LAMINATES;
GLASS FIBER REINFORCED PLASTICS;
COMPOSITE LAMINATE;
DYNAMIC MECHANICAL ANALYSIS (DMA);
DYNAMIC SHEAR MODULUS;
LINEAR THERMAL EXPANSION COEFFICIENTS;
MEASUREMENT METHODOLOGY;
MECHANICAL CHARACTERISTICS;
SIMULATION RESEARCH;
TEMPERATURE DIFFERENCES;
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EID: 0031988207
PISSN: 02728397
EISSN: None
Source Type: Journal
DOI: 10.1002/pc.10076 Document Type: Article |
Times cited : (11)
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References (7)
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