FE method, how ? (software Comsol)

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SUMMARY

The discussion focuses on the implementation of the plastic flow rule for large strains in continuum mechanics using COMSOL Multiphysics. The flow rule is expressed mathematically, and the process of computing plastic state variables at Gauss points is clarified. Key steps include the elastic predictor and plastic corrector methods, which utilize a damped Newton method for solving nonlinear systems. The distinction between Gauss points and mesh nodes is emphasized, as Gauss points are internal to the elements used in finite element analysis.

PREREQUISITES
  • Understanding of plastic flow rules in continuum mechanics
  • Familiarity with COMSOL Multiphysics software
  • Knowledge of finite element analysis and Gauss quadrature
  • Basic principles of nonlinear system solving, particularly damped Newton methods
NEXT STEPS
  • Study the implementation of plastic flow rules in COMSOL Multiphysics
  • Learn about Gauss quadrature and its application in finite element analysis
  • Explore nonlinear system solving techniques, focusing on damped Newton methods
  • Investigate the relationship between boundary conditions and deformation gradients in continuum mechanics
USEFUL FOR

This discussion is beneficial for mechanical engineers, finite element analysts, and researchers working on material behavior under large strains, particularly those utilizing COMSOL Multiphysics for simulations.

trabo
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Hi all,

The plastic flow rule for large strains in a continuum medium can be written as :
-\dfrac{1}{2} \Big ( \dfrac{d}{dt}(F_p^{-1} ). ^t F_p^{-1} + F_p^{-1} . ^t \dfrac{d}{dt} ( F_p^{-1} ) \Big)= \lambda F^{-1} \dfrac{\partial f}{\partial \tau} F F_p^{-1} . ^t F_p^{-1}
where F_p is the plastic part of the total deformation gradient F, f the yield surface and \tau the Kirchhoff stress tensor.
According to Comsol notes, we denote M=F_p^{-1} and discretize the law by using 'variations with \Delta' :
-\dfrac{1}{2} \Big [ 2M. ^t M -M_{old} . ^t M - M . ^t M_{old} \Big ]= \lambda \Delta t F^{-1} \dfrac{\partial f}{\partial \tau} FM. ^t M​
but I don't understand what is stated after. I quote :

For each Gauss point, the plastic state variables (ε_p and M, respectively) and the plastic multiplier,\Lambda =\lambda \Delta t, are computed by solving the above time-discretized flow rule together with the complementarity conditions
\Lambda \ge 0 \quad , \quad f \le 0 \quad , \quad \Lambda f = 0​
This is done as follows (Ref. 4):
1- Elastic-predictor: Try the elastic solution M= M_{old} and \Lambda=0. If this satisfies f \le 0 it is done.
2- Plastic-corrector: If the elastic solution does not work (this is f > 0), solve the nonlinear system consisting of the flow rule and the equation f=0 using a damped Newton method.

Few things I don't understand or I'm not sure of :

1/ Gauss points stand for the mesh nodes, right ?
2/ What does "For each Gauss point the plastic strain variables are computed" mean ? We have matrices that describe the body state at all his points, that is, there is not a matrix for each point of the body, so I don't understand the beginning of their sentence.
3/ The total deformation gradient F is also a variable, we don't know its value, so how the computing is done for M

Regards
 
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For the third point, does F depend on the boundary conditions ? For instance, if we consider a round tensile specimen with prescribed displacement at the top and below surface and with free stress on the lateral surface, can we infer F ?
Sure, we know its impqct on points at the top and below surface, but can we infer all its components ? If the total displacement vector is known at the two outer surfaces, then yes we can know all components of F, but if only the radial displacement is prescribed, some components can not be determined
 
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trabo said:
Few things I don't understand or I'm not sure of :

1/ Gauss points stand for the mesh nodes, right ?
2/ What does "For each Gauss point the plastic strain variables are computed" mean ? We have matrices that describe the body state at all his points, that is, there is not a matrix for each point of the body, so I don't understand the beginning of their sentence.
3/ The total deformation gradient F is also a variable, we don't know its value, so how the computing is done for M

Regards

No, the Gauss points are no the mesh nodes. The Gauss Points, or Gaussian Integration Points, are internal to the elements. More can be found here (last paragraph of the page marked 11) and http://www.colorado.edu/engineering/cas/courses.d/IFEM.d/IFEM.Ch28.d/IFEM.Ch28.pdf.
 

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