Experimental building block approach and numerical modelling of thermoplastic composite used for fuselage panels
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The present work focuses on the experimental and numerical investigation of thermoplastic composite
aircraft structures through a building block approach [1-3]. Numerical simulations take part as to
derive a preliminary behavior of the thermoplastic composite material and extract the optimum
geometry and stacking sequence and then validation comes from the experimental campaign. The tests
are extended from material characterization coupons to the demonstrator multistiffener panel
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