Rubber Ball Impacts on Composite Plates Investigation by 3D Correlation

P. Guégan; R. Othman; F. Pasco; N. Swiergiel; P. Thévenet; J.M. Guimard

doi:10.4028/www.scientific.net/AMM.566.397

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 566Rubber Ball Impacts on Composite Plates...

Rubber Ball Impacts on Composite Plates Investigation by 3D Correlation

Abstract:

Aircraft structures and wings should endure tyre debris impacts. Therefore, numerical simulations which are able to predict such phenomena are highly appreciated for the aircraft structures design. However these simulations have to be developed, tuned and validated by means of experimental data. Nowadays, full-scale tests are widely used. However, they include too complex mechanisms, which are difficult to consider in a process of model development. Besides, these experiments are extremely expensive. In this work, we are dealing with a simplified experimental set-up with elementary boundary conditions. Namely, we are experimentally investigating rubber balls’ impact on composites panels. The main novelty is the use of 3D-stereo correlation technique.

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Periodical:

Applied Mechanics and Materials (Volume 566)

Pages:

397-402

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.566.397

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Online since:

June 2014

Authors:

P. Guégan*, R. Othman, F. Pasco, N. Swiergiel, P. Thévenet, J.M. Guimard

Keywords:

3D Correlation, Aircraft Structures, Impact, Tyre Debris

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References

[1] R.A.W. Mines, S. McKown and R.S. Birch: Int. J. Impact Eng. Vol. 34 (2007), p.627.

Google Scholar

[2] D. Karagiozova and R.A.W. Mines: Int. J. Impact Eng. Vol. 34 (2007), p.647.

Google Scholar

[3] P. Guégan, R. Othman, D. Lebreton, F. Pasco, N. Swiergiel and P. Thevenet: Int. J. Crashworthiness, Vol. 15, N°4, August 2010, p.391.

DOI: 10.1080/13588260903504044

Google Scholar

[4] P. Guégan, R. Othman, D. Lebreton, F. Pasco, N. Swiergiel, P. Thevenet, B. Malherbe and J. Maffre: International DYMAT Conference, Brussels, Belgium, 7-11/09/2009, DOI: 10. 1051/Dymat/2009075, p.525.

DOI: 10.1051/dymat/2009075

Google Scholar

[5] R. Othman: Strain 48 (2012), p.16.

Google Scholar

[6] P. Guégan, R. Othman, D. Lebreton, F. Pasco, P. Villedieu, J. Meyssonnier and S. Wintenberger: Int. J. Impact Eng. Vol. 38 (2011), p.786.

DOI: 10.1016/j.ijimpeng.2011.05.003

Google Scholar

[7] P. Guégan, R. Othman, D. Lebreton, F. Pasco, P. Villedieu, J. Meyssonnier and S. Wintenberger: Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci. 226 (2012), p.1677.

DOI: 10.1177/0954406211426639

Google Scholar

[8] http: /www. lavision. de/en/products/davis. php.

Google Scholar