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- W2373520101 abstract "Composite overwrapped pressure vesseles(COPV)are widely applied to space system.Finite element model of COPV and its liner are established by ANSYS finite element program.In the modeling,the total of filament wind ing layers are handled as composite laminate,with considering variational thickness and wrap angle of every unidirection al layer of the domes.Eigen buckling and nonlinear buckling finite element equations o f the integral vessel are established.Buckling cal-culation of COPV and its liner are respectively made,and buckling modal s hapes and the critical outer pressur e are obtained。" @default.
- W2373520101 created "2016-06-24" @default.
- W2373520101 creator A5044647798 @default.
- W2373520101 date "2005-01-01" @default.
- W2373520101 modified "2023-09-25" @default.
- W2373520101 title "FINITE ELEMENT MODELING AND BUCKLING ANALYSIS OF COPV" @default.
- W2373520101 hasPublicationYear "2005" @default.
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