Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Two contiguous rigid bodies

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Example shell element reference frame rl and Al=[xl yl zl]

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: The interpolation points for the out-of-plane shear strains of the MITC4

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Cantilever model with plastic material and hexahedral element formulation. Traction load applied to free end. Displacement compared at point marked . Von Mises stress compared at point marked . (Model with 10 mm elements shown).

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Distributed edge pressure load applied in the vertical direction to free end of cantilever plate model

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Displacement of node at free end of cantilever, (a) time 0 to −2 sec, and (b) time 1.9 to −2.0 sec, for element sizes 2.5 and 5 mm, for abaqus™ (Ab) and the proposed formulation (Pr), for hexa-type solid elements

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: von Mises stress of node near base of cantilever, (a) time 0 to −2 sec, and (b) time 1.9 to −2.0 sec, for element sizes 2.5 and 5 mm, for abaqus™ (Ab) and the proposed formulation (Pr), for hexa-type solid elements

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: The model used for verification of the hyperelastic material behavior

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Total force applied to Force applied to the free end of the hyperelastic model

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: (a) x-displacement and (b) von Mises stress of proposed versus. abaqus™ model for a Mooney–Rivlin material

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: A test model including rigid bodies modeled with the recursive formulation and flexible bodies that use plasticity and hyperelasticity

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Configuration of the mechanism model between times 0.0 and 3.0 sec

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Magnitude of contact forces between bodies B and E and between bodies C and E

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: Equivalent von Mises strain for total and plastic strain components on the top (inside of curvature after deformation) and bottom (outside of curvature after plastic deformation) of body E at the point of maximum strain

Date of download: 12/20/2017 Copyright © ASME. All rights reserved. From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity J. Comput. Nonlinear Dynam. 2014;9(4):041012-041012-11. doi:10.1115/1.4027580 Figure Legend: von Mises stress at a node near the midpoint of body F (hyperelastic body)