Joel Serra’s Post

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Research Engineer in Composite Materials Mechanics

The certification of large composite structures is based on a pragmatic approach, which is intended to be safe and essentially experimental but with a strong test/calculation dialogue called the “Test Pyramid”.   However, this has proved to be extremely expensive and it appears necessary to reduce its cost either by developing Virtual testing, or by developing richer tests on an intermediate scale between coupon specimens and structural parts.   It was in the aim of meeting this objective that the VERTEX program (French acronym for “Experimental modeling and Validation of compositE strucTures under complEX loading”) was launched in 2012. The 5-year VIRTUOSE program (https://lnkd.in/endtpCix) started in 2019 made it possible to develop further the Tests/Measurement/Numerical Simulation tryptic.   In this paper, we summarize more than 12 years of research ! This is a joint effort with my colleagues from Institut Clément Ader (ICA) CNRS UMR 5312 Bruno CASTANIÉ christophe bouvet Jean-Charles Passieux Jean-Noel Périé and John-Eric Dufour.   The article is in Open Access mode : https://lnkd.in/efB7U5zr   #correlation #image #testing #compositematerials #structural

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Lionel Juillen

Aerospace Structural Analyst - Finite Element and Optimisation Specialist

7mo

Thanks for sharing the link to the pre-proff version of the paper... Page 4 (paragraph 2) the maximum load enveloppe for pure tension/compression is 3000 N/m and 1000 N/mm for shear.. When we have combined loadings what could be the highest values of combinations ? (e.g. in Ref 5, of the paper we can find some load cases : 1000 N/mm for tension/compression combined with 1000 N/mm for shear). is 1000 N/mm the max value for tension/compression when combined with the max shear load value ? Regards

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Germain Boudinet

Optimist Optimizer | Aero ✈️, Space 🛰️ and Additive Manufacturing 🌿

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