VUMAT subroutine: 3D Hashin failure criteria in Abaqus with exponential damage evolution

Rated 5.00 out of 5 based on 1 customer rating

$ 399.00

3D Hashin failure criteria in Abaqus with exponential damage evolution

Name: VUMAT subroutine: 3D Hashin failure criteria in Abaqus with exponential damage evolution
Brand: FEA simulation consulting
SKU: 010
Price: 399 USD
Availability: InStock
Rating: 5 (178 reviews)

In order to effectively describe the progressively intralaminar and interlaminar damage for composite laminates, a three-dimensional progressive damage model for composite laminates to be used for low-velocity impact is presented. it is based on continuum damage mechanics (CDM) and was developed and implemented in the user subroutine of ABAQUS explicit, VUMAT. the nonlinear damage model can be used to analyze the dynamic performance of the composite structure and its failure behavior. For the intralaminar damage, as a function of the energy release rate, the damage model in an exponential function can describe the progressive development of the damage. VUMAT subroutine is validated by well-known papers and can be used in any simulation.

Abaqus hashin example:

This project and similar projects have been reviewed for َAbqus Hashin damage models in various materials such as composites. Our engineering team has the ability to design and perform similar calculations, and you can contact our expert team via email and the site.

Hashin damage Abaqus is commonly used in fiber-reinforced composite materials.
Hashin damage model in Abaqus software has 4 different models:

Fiber stretch
Fiber compression
Matrix traction
Matrix compression

Tensile test validation (*.cae, *.inp, *.jnl, *.odb)
Compression test validation (*.cae, *.inp, *.jnl, *.odb)
Shear test validation (*.cae, *.inp, *.jnl, *.odb)
3D Hashin VUMAT Subroutine with exponential damage evolution (*.for, *.f)
User manual (*.pdf)
Guarantee up to 3 years

Out of stock

VUMAT Subroutine for

3D Hashin failure criteria in abaqus explicit

Abaqus Explicit-Damage initiation by Abaqus Hashin criterion

abaqus explicit

3D Hashin Failure criterion is not supported in abaqus explicit for solid elements. The Hashin damage initiation criterion must be used with elements with a plane stress formulation, which includes plane stress, shell, continuum shell, and membrane elements. so it is not used for 3D solid elements. It is often necessary to use 3D solid elements (For example C3D8R) in simulating the damage of FRP composite materials with an explicit solver. So what is the solution?

The Abaqus anisotropic damage model for unidirectional fiber-reinforced composite is based on the work of Matzenmiller et al. (1995), Hashin and Rotem (1973), Hashin (1980), and Camanho and Davila (2002).

Four different modes of failure are considered:

fiber rupture in tension;
fiber buckling and kinking in compression;
matrix cracking under transverse tension and shearing; and
matrix crushing under transverse compression and shearing.

Damage evolution for fiber-reinforced composites in Abaqus

it is based on energy dissipation during the damage process and is linear. in the following table, you can find the differences between Abaqus built-in Hashin model and the 3D Hashin VUMAT subroutine.

	Abaqus built-in Hashin	3D Hashin VUMAT Subroutine
Elements	Plane stress, shell, continuum shell, and membrane elements	Three-dimensional solid element
Damage Initiation	Hashin and Rotem (1973), Hashin (1980)	Hashin (1980) and Maximum stress criteria
Damage Evolution	Linear	Exponential (based on Linde (2004))
Remove Elements	yes	yes
Solver	Standard & Explicit	Explicit

my shop

For all Abaqus users
Validated
Nonlinear progressive damage model
Exponential damage variables

Removing failed elements
Reduce mesh sensitivity by introducing characteristic elements
Dynamic & quasi-static simulations

Special features

Subroutine: VUMAT
Software: Abaqus
Damage initiation: Hashin (1980) & maxixmum stress
Damage evolution: Linde (2014)
Verified: Yes
Guarantee: 3 years
Documented: Yes

Mesh sensitivity:: reduced by introducing characteristic length
Precision: single & double
HPC: Yes
OS: Linux & Windows
Solver: Explicit
Material: composite laminates

3D Hashin VUMAT Subroutine

Material

Better prediction of progressive damage of lamionated composites

Delamination

Apply cohesive elements in 3D solid

Mesh sensitivity

The energy dissipation and characteristic length are introduced into the damage evolution law to reduce the mesh sensitivity

Damage variables

7 damage variables to see every mode of failure

Shear modes

It is based on the maximum stress criterion. Also, shear stiffness loss due to the matrix failure under loading is investigated.

Global damage variables

it is also applied to separate fiber and matrix failures.

How to find us

Toos Industrial Zone, Mashhad
Phone: (+98)51-35424520
Email: info@BanuMusaGr.com

We are ready to help you do CFD & FEA simulations.

Need help? Get a consultation from our experts.

Email us: info@banumusagr.com
Telegram: +98-915-55-20-388
WhatsApp: +98-915-55-20-388

Software

Abaqus SIMULIA, Subroutines

Type

Tutorial + VUMAT + documentation

Files

*.cae, *.jnl, *.inp, *.odb, *.for, *.f, *.odb, *.pdf,

Language

Fortran

VUMAT subroutine: 3D Hashin failure criteria in Abaqus with exponential damage evolution

3D Hashin failure criteria in Abaqus with exponential damage evolution

Abaqus hashin example:

Contents

3D Hashin failure criteria in abaqus explicit

Abaqus Explicit-Damage initiation by Abaqus Hashin criterion