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The composite material for the board is a fiber-reinforced laminate structure.
The design of the laminate structure of the CFRP is then optimized, considering various laminate processes.
Thicker laminate structure in new commercial passenger aircraft will affect maintainability.
The weakest parts of a composite laminate structure are often the joints.
The model accounts for geometric nonlinearities and the composite laminate structure.
Present research is focused on numerical and experimental investigation of glass laminate structure consolidated with ethylene vinyl acetate film.
Similar(30)
This model requires a non-linear laminate theory which provides the response of laminate structures.
This paper presents two alternative approaches for realizing weight-minimal laminate structures by topology optimization.
The problem of uncertainty propagation in composite laminate structures is studied.
Two examples of laminate structures show the effectiveness of the proposed algorithms.
This paper presents the design optimization of thin-walled composite laminate structures to maximize stiffness at minimum material cost.
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