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108
ANSYS钢筋混凝土建模(FINITE ELEMENT MODELING OF REINFORCED CONCRETE STRUCTURES STRENGTHENED WITH FRP
LAMINATES
)
.pdf
FINITEELEMENT MODELING OFREINFORCED CONCRETE STRUCTURESSTRENGTHENED FRPLAMINATESFinal ReportSPR 316O
建筑之家
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顶
2
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3
Dimensional Stability, Glass Reinforced Thin
Laminates
.pdf
1.0Scope proceduredefines testmethod used todetermine dimensional stability glassreinforced, copper-
cjejia56
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85
ar00-46 Repair of Composite
Laminates
.pdf
ar00-46 Repair of Composite Laminatesar00-46 Repair of Composite Laminatesar00-46 Repair of Composite Laminates
blueangel
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10
Accelerated hygrothermal cyclical tests for carbonepoxy
laminates
.pdf
The paper deals with the design of reasonable accelerated test conditions to assess polymer matrix composite durability when it is
subjected to supersonic flight-cycles. The study is closely linked to novel application of carbon fibre polymer matrix composites in
supersonic aircraft primary structures, leading to substantial weight saving and stiffness improvement. A supersonic flight can result in
surface temperatures close to 130 8C, inducing severe thermal gradients and drying which are quite new for this type of materials, now used
in primary structures of subsonic jets operating at low subsonic flight-temperatures. Therefore, the particular effect of the drying on the longterm
behaviour of composites should be investigated. Numerical simulations based on Fick’s law confirm that the supersonic flight-cycles
induce a material drying on the long-term and a significant moisture uptake occurs during the aircraft maintenance periods. Then, particular
accelerated cycles are proposed
t497701228
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19
modelling and simulation of fibre metal
laminates
.pdf
2004ABAQUS Users’ Conference 421 Modelling FibreMetal Laminates Peter Linde1, Jrgen Pleitner1, Henk
apanghuang32
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143
gas transport in out-of-autoclave prepreg
laminates
.pdf
gas transport in out-of-autoclave prepreg laminates
jingqdrb
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