1. Date of download: 12/20/2017
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From: Systematic Integration of Finite Element Methods Into Multibody Dynamics Considering Hyperelasticity and Plasticity
J. Comput. Nonlinear Dynam. 2014;9(4): doi: /
Figure Legend:
Two contiguous rigid bodies

2. 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): doi: /
Figure Legend:
Example shell element reference frame rl and Al=[xl yl zl]

3. 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): doi: /
Figure Legend:
The interpolation points for the out-of-plane shear strains of the MITC4

4. 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): doi: /
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).

5. 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): doi: /
Figure Legend:
Distributed edge pressure load applied in the vertical direction to free end of cantilever plate model

6. 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): doi: /
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

7. 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): doi: /
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

8. 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): doi: /
Figure Legend:
The model used for verification of the hyperelastic material behavior

9. 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): doi: /
Figure Legend:
Total force applied to Force applied to the free end of the hyperelastic model

10. 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): doi: /
Figure Legend:
(a) x-displacement and (b) von Mises stress of proposed versus. abaqus™ model for a Mooney–Rivlin material

11. 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): doi: /
Figure Legend:
A test model including rigid bodies modeled with the recursive formulation and flexible bodies that use plasticity and hyperelasticity

12. 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): doi: /
Figure Legend:
Configuration of the mechanism model between times 0.0 and 3.0 sec

13. 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): doi: /
Figure Legend:
Magnitude of contact forces between bodies B and E and between bodies C and E

14. 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): doi: /
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

15. 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): doi: /
Figure Legend:
von Mises stress at a node near the midpoint of body F (hyperelastic body)