Carbon Fiber Reinforced Polymer (CFRP) composites are well established in aircraft, aerospace and automotive industry due to their lightweight structure and robustness. Generally, in uni-directional (UD) composite laminates the mechanical properties depend of fiber orientation, the number and the thickness of the plies and the stacking sequence [1], Fig. 1. In continuous fiber laminates the prediction of failure is dependent on the fiber orientation and the failure criteria that are adopted.
Russo, M., Pappa, E., Baroni, A., Corvaglia, S., Lopresto, V., Papa, I. (2024). Low Velocity Impact (LVI) Simulation of a CFRP Ply-Drop Laminates: A Numerical Analysis, 1, 102-116 [10.1007/978-3-031-77697-7_13].
Low Velocity Impact (LVI) Simulation of a CFRP Ply-Drop Laminates: A Numerical Analysis
Russo M.
Co-primo
;
2024
Abstract
Carbon Fiber Reinforced Polymer (CFRP) composites are well established in aircraft, aerospace and automotive industry due to their lightweight structure and robustness. Generally, in uni-directional (UD) composite laminates the mechanical properties depend of fiber orientation, the number and the thickness of the plies and the stacking sequence [1], Fig. 1. In continuous fiber laminates the prediction of failure is dependent on the fiber orientation and the failure criteria that are adopted.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
