Reference : Experimental characterization and constitutive modeling of TA6V mechanical behavior in p...
Scientific congresses and symposiums : Paper published in a journal
Engineering, computing & technology : Materials science & engineering
http://hdl.handle.net/2268/115628
Experimental characterization and constitutive modeling of TA6V mechanical behavior in plane strain state at room temperature
English
Gilles, Gaëtan mailto [Université de Liège - ULg > Département Argenco : Secteur MS2F > Département Argenco : Secteur MS2F >]
Tuninetti Vásquez, Victor mailto [Université de Liège - ULg > Département Argenco : Secteur MS2F > Département Argenco : Secteur MS2F >]
Ben Bettaieb, Mohamed mailto [Université de Liège - ULg > Département Argenco : Secteur MS2F > Département Argenco : Secteur MS2F >]
Cazacu, O. [University of Florida REEF > Department of Mechanical and Aerospace Engineering > > >]
Habraken, Anne mailto [Université de Liège - ULg > Département ArGEnCo > Département ArGEnCo >]
Duchene, Laurent mailto [Université de Liège - ULg > Département Argenco : Secteur MS2F > Analyse multi-échelles des matériaux et struct. du gén. civ. >]
2011
AIP Conference Proceedings
American Institute of Physics
1383
Yes (verified by ORBi)
International
0094-243X
8th International Conference and Workshop on Numerical Simulation of 3D Sheet Metal Forming Processes
August 21-26 2011
Seoul
Korea
[en] TA6V titanium alloy ; material anisotropy ; strength differential effect ; anisotropic yield criterion ; LIMARC
[en] This paper presents an experimental and theoretical study of the quasi-static behavior of TA6V titanium alloy in plane strain state. In order to quantify the anisotropy of the material, tests were carried out at room temperature on specimens cut out from a sheet along three loading directions. The initial yield locus is described by the phenomenological CPB06ex3 criterion and Voce’s type isotropic hardening is used. Finite element simulations are performed and compared with the experiments.
http://hdl.handle.net/2268/115628

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