Numerical simulations and testing of notched composite plates under envelope loadings: Validation with the safe life domain method

Author:

Grotto FlorentORCID,Bouvet ChristopheORCID,Castanié BrunoORCID,Serra JoëlORCID

Publisher

Elsevier BV

Reference41 articles.

1. Rouchon J. Certification of Large Airplane Composite Structures Recent Progress and New Trends in Compliance Philosophy. In: Proceedings of ICAS 2 (1990), pp. 1439-1447. https://www.icas.org/ICAS_ARCHIVE/ICAS1990/ICAS-90-1.8.1.pdf.

2. Thomsen O, Dulieu-Barton J, Halett S, Butler R. Validation of composite aerostructures through integrated multi-scale modelling and high-fidelity substructure testing facilitated by design of experiments and bayesian learning. In: Proceedings of the European conference on composite materials, ECCM 20, Lausanne, Switzerland, June 26-30; 2022.

3. Testing structural elements under multiaxial loading: a numerical model of the bench to understand and predict complex boundary conditions;Grotto;Aerospace,2024

4. Validation and modeling of aeronautical composite structures subjected to combined loadings: the VERTEX Project, Part 1: Experimental setup, FE-DIC instrumentation and procedures;Serra;Comp Struct,2017

5. Validation of aeronautical composite structures under multiaxial loading: the VERTEX Project, Part 2: Load envelopes for the assessment of panels with large notches;Serra;Comp struct,2017

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