Proceedings of the ... International Conference on Offshore Mechanics and Arctic Engineering, Volume 18, Part 3American Society of Mechanical Engineers, 2000 - Arctic regions |
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Page 191
The multiaxial stress interaction parameter k for a fiber reinforced composite may may be determined from the consideration of material strength anisotropy and composite fatigue experiments . The physical significance of k in a fiber ...
The multiaxial stress interaction parameter k for a fiber reinforced composite may may be determined from the consideration of material strength anisotropy and composite fatigue experiments . The physical significance of k in a fiber ...
Page 202
... fibers Fiber Density E - modulus ( g / cm3 ) ( GPa ) Strain to failure ( % ) E - glass 2.62 80 4.6 Carbon 1 1.80 234 1.9 Carbon 2 1.80 230 2.1 Aramid 1 1.45 121 2.0 Aramid 2 1.45 135 2.8 .. 1 Property PVDF PK PEX PA Temp . C 20 60 23 80 ...
... fibers Fiber Density E - modulus ( g / cm3 ) ( GPa ) Strain to failure ( % ) E - glass 2.62 80 4.6 Carbon 1 1.80 234 1.9 Carbon 2 1.80 230 2.1 Aramid 1 1.45 121 2.0 Aramid 2 1.45 135 2.8 .. 1 Property PVDF PK PEX PA Temp . C 20 60 23 80 ...
Page 207
... fiber materials together with the matrix material . In general , the higher the elastic modulus of the fiber the better the fatigue capacity . Based on this , a carbon fiber laminate would be beneficial . However , this tube is to be ...
... fiber materials together with the matrix material . In general , the higher the elastic modulus of the fiber the better the fatigue capacity . Based on this , a carbon fiber laminate would be beneficial . However , this tube is to be ...
Contents
STRUCTURAL INTEGRITY PROCEDURES FOR EUROPE SINTAP | 1 |
OMAE99MAT2041 | 9 |
Development of the SINTAP Failure Assessment Diagrams for Compatibility With | 19 |
Copyright | |
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addition analysis applications approach ASME assessment base behavior bending CGHAZ Charpy compared component composite condition Conference Copyright crack critical CTOD curve defects deposition depth determined developed distribution dynamic effect element energy Engineering equations equivalent evaluated factors failure fatigue ferrite Figure fire fracture toughness function geometry given hardness heat input impact important improve increase initiation International joints length limit loading lower material matrix maximum mean measured mechanical method microstructure molten observed obtained offshore operating parameters performance phase pipe plate prediction present pressure procedure production properties protection range ratio reduced region requirements residual stress respectively risers safety ship shown shows specimens standards steel strain strength structures surface Table temperature tensile thickness values weld metal welded joints wire yield