The P–h2 relationship on load–displacement curve considering pile-up deformation mode in instrumented indentation by Habibi, S., Chicot, D., Mejias, A., Boutabout, B., Zareb, E., Semsoum, D. E., Benaissa, S., Mezough, A., Merzouk, H.

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Numerical analysis of the performances of bonded composite repair with two adhesive bands in aircraft structures by Fekirini, H., Bachir Bouiadjra, B., Belhouari, M., Boutabout, B., Serier, B.

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Fracture energy for repaired cracks with bonded composite patch having two adhesive bands in aircraft structures by Bachir Bouiadjra, B., Fekirini, H., Belhouari, M., Boutabout, B., Serier, B.

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Computation of the stress intensity factor for patched crack with bonded composite repair in pure mode II by Megueni, A, Bachir Bouiadjra, B, Boutabout, B

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Junction Ni/Al2O3 Elaborated by Thermocompression: Determination of the Thermal Residual Stresses by Boutabout, B, Serier, B, Bouiadjra, B B, Treheux, D

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Numerical Study of the Effect of the Penetration of a Crack in the Matrix of a Composite by Nehari, T., Ziadi, A., Ouinas, D., Boutabout, B.

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Effect of thermomechanical loads on the propagation of crack near the interface brittle/ductile by Boutabout, Benali, Chama, Mourad, Bouiadjra, Bel Abbes Bachir, Serier, Boualem, Lousdad, Abdelkader

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Junction Ni/Al 2 O 3 Elaborated by Thermocompression: Determination of the Thermal Residual Stresses by BOUTABOUT, B., SERIER, B., BOUIADJRA, B. BACHIR, TRÉHEUX, D.

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