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  1. Material
  2. Material3D
  3. Concrete

CDPM2

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Last updated 1 year ago

CDPM2 Model for Concrete Material

References

Syntax

material CDPM2 (1) [2-16]
material CDPM2ISO (1) [2-16]
material CDPM2ANISO (1) [2-16]
# (1) int, unique material tag
# [2] double, elastic modulus, default: 3E4
# [3] double, poissons ratio, default: 0.3
# [4] double, tension strength (positive), default: 3.0
# [5] double, compression strength (positive), default: 30.0
# [6] double, q_h0, initial hardening factor, default: 0.3
# [7] double, h_p hardening ratio, default: .01
# [8] double, d_f, default: .85
# [9] double, a_h, hardening related parameter, default: 0.08
# [10] double, b_h, hardening related parameter, default: 0.003
# [11] double, c_h, hardening related parameter, default: 2.0
# [12] double, d_h, hardening related parameter, default: 1E-6
# [13] double, a_s, ductility related parameter, default: 5.0
# [14] double, e_ft, tension softening parameter, default: 5E-4
# [15] double, e_fc, compression softening parameter, default: 5E-4
# [16] double, density, default: 0.0

Remarks

  1. The isotropic damage is implemented.

  2. The anisotropic damage is implemented.

  3. The default CDPM2 uses isotropic damage, which is equivalent to CDPM2ISO.

  4. The token CDPM2ANISO uses anisotropic damage.

  5. If damage is activated, both tension and compression use the exponential damage model, the degradation is controlled by parameters [14] and [15]. The characteristic length can be accounted for by modifying them.

Recording

This model supports the following additional history variables to be recorded.

variable label
physical meaning

DT

tensile damage

DC

compressive damage

Examples

The isotropic damage uses the following expression for the final stress σ\mathbf{\sigma}σ,

σ=(1−ωc)(1−ωt)σˉ.\mathbf{\sigma}=(1-\omega_c)(1-\omega_t)\mathbf{\bar{\sigma}}.σ=(1−ωc​)(1−ωt​)σˉ.

The anisotropic damage uses the following expression,

σ=(1−ωc)σˉc+(1−ωt)σˉt.\mathbf{\sigma}=(1-\omega_c)\mathbf{\bar{\sigma}}_c+(1-\omega_t)\mathbf{\bar{\sigma}}_t.σ=(1−ωc​)σˉc​+(1−ωt​)σˉt​.

In the above expressions, σˉ\mathbf{\bar{\sigma}}σˉ is the effective stress (undamaged), σˉc\mathbf{\bar{\sigma}}_cσˉc​ and σˉt\mathbf{\bar{\sigma}}_tσˉt​ are compressive and tensile part of the effective stress. They are computed via eigen decomposition of the effective stress tensor. ωc\omega_cωc​ and ωt\omega_tωt​ are the compressive and tensile damage variables, respectively.

Both damage types have physical implications. Depending on the damage type, the model parameters may be adjusted differently.

The reference strains efte_{ft}eft​ and efce_{fc}efc​ affect the degradation of strength.

The following are two examples, using different values of efte_{ft}eft​ and efce_{fc}efc​, while all other parameters are the default values.

For detailed explanations of parameters, please refer to .

Details of implementation can be seen in the corresponding section in .

10.1016/j.ijsolstr.2013.07.008
10.1016/j.ijsolstr.2005.05.038
10.1016/j.ijsolstr.2013.07.008
Constitutive Modelling Cookbook
compressive
tensile