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Puck damage criterion | Puck failure criterion
HomeCivil Engineering Simulation of composite Puck damage in 3d continuum element in Abaqus (UMAT-USDFLD-VUMAT)
Produced in Partnership Plan

Simulation of composite Puck damage in 3d continuum element in Abaqus (UMAT-USDFLD-VUMAT)

€ 250

In this training package, the 3D continuum puck damage initiation model is prepared via three subroutines (USDFLD, UMAT and VUMAT).This training package teach you subroutines line-by-line. It should be noted that after damage initiation, failure occurs suddenly and in the form of a reduction in properties in the model.

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Description

Simulation of composite Puck damage in 3d continuum element in Abaqus (UMAT-VUMAT-USDFLD)

This training package focuses on the Puck failure/puck damage criterion in a simple 3d element example using helpful subroutines in Abaqus.

Introduction to Puck failure criterion

An interactive stress-based criterion for failure, Puck’s failure criterion (Puck and Schürmann 1998; Puck, Kopp, et al. 2001; Puck and Schürmann 2001) is appropriate for UD (unidirectional) composite lamina (plies). Puck damage is a kind of composite failure criterion that have some advantages and disadvantages.
The failure is brought on by normal and shear forces acting on the fracture plane at an angle to the material plane, according to the Mohr-Coulomb assumption that forms the basis of the Puck criterion. The Puck theory may anticipate two types of failure: fiber failure and inter-fiber failure. Puck’s description of the inter-fiber failure is essentially matrix cracking.

The inter-fiber failure criterion is based on the presumption that only stresses acting on the fracture plane can cause a fracture (Puck damage assumptions). The fracture plane can be angled between -90 and +90 degrees with regard to the material plane. By moving the three-dimensional stress tensor from the material coordinate system to the fracture plane using the common tensor transformations, the normal and shear stresses operating on this plane are determined.

Failure degradation

The local characteristics are reduced in accordance with the failure type indicated by the failure criterion when the failure is expected by the failure criteria in a specific position of the composite component. Over the past few years, a wide range of degradation models has been put forth (Craddock 1982; Chang, Scott et al. 1984; Gamble, Pilling et al. 1995). According to Murray (1990), there are three basic categories into which degrading material models can be divided: instantaneous, gradual unloading, and constant stress. In this training package, we use instantaneous degradation.

The Abaqus user subroutine allows the program to be customized for particular applications unavailable through the main Abaqus facilities. You should write a user subroutine if you could not run your analysis by ABAQUS built-in models for materials, loads, properties, elements, etc. for example, if you need to model a user-defined nonlinear stress-strain relation, which is not provided by Abaqus, then look for UMAT user subroutine. A more simple subroutine is USDFLD, which allows the creation of user-defined parameters. If it is your first time writing a subroutine like UMAT, VUMAT or USDFLD please read the Start Writing an Abaqus Subroutine: Basics & Recommendations article. After reading this post and watching this tutorial’s demo video, you will definitely decide to save time in Abaqus modelling and get this training package. If you have questions, ask here on our live chat on the left.

It would be useful to see Abaqus Documentation to understand how it would be hard to start an Abaqus simulation without any Abaqus tutorial. If you are working on Abaqus composite damage and need resources about composite FEM simulation, click on the Abaqus composite analysis page to get more than 20 hours of video training packages of composite materials simulation.

After purchase, you can access the software files and subroutines immediately.

The video files will be available 2 months later after purchase.

Preview

  • What do we learn from this package?
  • Teaching plan and Prerequisites and Next steps
  • Package specification

Introduction

  • How to model 3d composite materials in ABAQUS?
  • What are the different types of damage initiation criteria for composite materials in ABAQUS?
  • What is the difference between sudden and gradual degradation of mechanical properties for composite materials in ABAQUS?
  • Introduction to different damage initiation and progressive damage theories and equations for composite materials.

Workshop-1 part-1:Simulation of composite Puck damage in 3d continuum element in Abaqus with UMAT

  • Problem Description
  • Description of Puck Theory
  • UMAT Puck subroutine flowchart
  • Writing the subroutine line by line
  • Simulation of plate under different loading (all modulus) with UMAT subroutine
  • Simulation of plate under different loading (all modulus) without subroutine(Standard solver)
  • Simulation of plate under different loading (all modulus) without subroutine(Explicit solver)
  • UMAT Hashin Subroutine validation with Abaqus solvers (Standard and explicit)

Workshop-1 part-2: Simulation of composite Puck damage in 3d continuum element in Abaqus with VUMAT

  • Problem Description
  • Description of Puck Theory
  • VUMAT Puck subroutine flowchart
  • Writing the VUMAT puck subroutine line by line
  • Simulation of plate under different loading (all modulus) with VUMAT subroutine
  • Simulation of plate under different loading (all modulus) without subroutine(Standard solver)
  • Simulation of plate under different loading (all modulus) without subroutine(Explicit solver)
  • Subroutine validation with Abaqus solvers (Standard and explicit)

Workshop-1 part-3: Simulation of composite Puck damage in 3d continuum element in Abaqus with USDFLD

  • Problem Description
  • Description of Puck Theory
  • USDFLD subroutine flowchart
  • Writing the subroutine line by line
  • Simulation of plate under different loading (all modulus) with USDFLD subroutine
  • Simulation of plate under different loading (all modulus) without subroutine(Standard solver)
  • Simulation of plate under different loading (all modulus) without subroutine(Explicit solver)
  • Subroutine validation with Abaqus solvers (Standard and explicit)
Additional information
Expert

Produced in Partnership Plan

Included

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

Tutorial video duration

160+ Minutes

language

English

Level

Advanced

Package Type

Training

Software version

Applicable to all versions

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SKU: AE5566-1-3 Categories: Civil Engineering, Composite, Fracture/Failure, Mechanical Enginerring, Subroutine Tags: ABAQUS, abaqus toturial collections, Composite, Puck, SUBROUTINE, UMAT, USDFLD, VUMAT

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