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 BEASY software provides a range of integrated software modules to help engineers perform fatigue crack growth analysis. BEASY can help your engineers improve their damage tolerance analysis work by providing them with tools to more accurately understand the behavior of flaws in critical structural components. Higher fidelity data characterizing critical crack sizes and crack growth rates will improve structural life estimates. If a crack is found during routine inspection a BEASY crack growth simulation can be used to determine if this crack will continue to grow and if so how much longer the asset can safely operate before repair is necessary. BEASY's automatic crack growth capability can also be used to support the non-destructive inspection (NDI) process. BEASY's crack path predictive capability can be used to guide NDI equipment operators to those fracture critical areas of the structure.

BEASY Fatigue & Crack Growth

BEASY's Fracture & Fatigue Crack Growth (FCG) software enables engineers to quickly develop high fidelity fracture mechanics models based on the actual structural component. This software is used by engineers, performing damage-tolerant design assessments, to determine accurate stress intensity factor (SIF) solutions and simulate 3D crack growth.

BEASY Crack Simulation Technology provides easy to use crack modelling tools to predict:

  • Stress Intensity Factors
  • Crack Growth Rates
  • Crack Growth Paths
  • Critical Crack Sizes

The BEASY SIF Wizard provides an interactive GUI that engineers can use to automatically insert, parametrically controllable crack shapes, in models.  Our easy to use modeling process supports the setup and launch of a FCG simulation using the BEASY Crack Growth Wizard - providing critical data on crack growth rates and crack shape evolution.

BEASY's Fracture Mechanics Software provides crack modelling tools to aid decision-making processes and discover potential problems at the design stage. BEASY advanced fracture mechanics software provides a radically improved approach to predictive computational analysis.

BEASY Automatic Crack Growth modelling technologies provides quick and accurate tools to:

  • Add cracks to models
  • Predict stress intensity factors
  • Predict crack growth rate and direction
  • Simulate crack growth in complex 3D structures
  • Predict residual strength

Automatic Crack Growth

The BEASY Crack Growth Wizard provides a process-driven GUI to launch fully automatic 3D crack growth simulations.  This system links the SIF solutions, fatigue crack growth material properties, and load spectrum to simulate crack growth in real structures.  The crack is advanced automatically based on user-defined parameters and provides information on how many cycles will be required to reach a critical crack size.

A variety of fatigue crack growth models, including the simple Paris Law, Walker Chang, and NASGRO can be selected. BEASY is fully integrated with the NASGRO 2, 3 material database and interfaces with later versions of NASGRO. The user can select the required material from a series of dropdown menus.

There is full support for using Load Spectrum (LSP) data to drive the crack growth process and a range of LSP formats are available; including standard block, sequential loading, and multi-axial load spectrum formats.

The SIF data and crack growth rate data can be quickly processed using graphing functions available in the Crack Growth Wizard or manipulated using BEASY's templates to display fatigue crack growth results in a series of charts and summary data tables using specially designed Excel macros. This data is also output in tabular formats for easy import into common desktop software.

Stress Intensity Factors

BEASY supports mixed mode crack growth and computes KI, KII and KIII.  The SIF is computed using either the J-Integral or Crack Opening Displacement (COD) method. BEASY provides a multi-point SIF solution along the entire crack front

Use The BEASY K-Solver To Feed Your Structural Lifing Software

The BEASY SIF Wizard is a powerful tool used to determine stress intensity factor solutions for cracks located in real geometry. The initial flaw can be selected from a library of crack shapes and automatically inserted in structural models. The SIF solution is determined along the entire crack front and is not just a two-point handbook type solution.  These SIF solutions can be effectively used to create a table of beta factor solution for commonly used engineering components. BEASY’s multi-point SIF solutions are critical for simulating accurate crack shape evolution and identifying critical locations along the crack front where fracture assessment criteria may be exceeded.

Damage Tolerant Design

Predict how cracks will impact the durability and integrity of a strcture during its service life:

  • What size crack will grow?
  • How fast will the crack grow?
  • How can the design be modified to increase durability and extend service life?
  • How will residual stress fields impact the crack growth rate?

Failure Investigation

Investigate the mode of failure by simulating crack growth behaviour:

  • In which direction will the crack propagate?
  • How will the part eventually fail?
  • How fast will the crack grow under existing operating conditions?
  • Is the "leak before break" criterion satisfied?
  • If a crack is discovered is it growing slow enough that it can be safely monitored by increasing the inspection interval?

Residual Stress Fields & Crack Growth Behaviour

Residual stresses are important as they can impact crack initiation locations and crack growth rates. Simulations can be used to avoid overly conservative designs and to understand where cracks may grow faster than expected. The BEASY modelling technology utilizes the residual stress field (often determined from FE nonlinear analysis) to drive the crack growth simulation.  A specialized methodology has been developed to accurately apply this stress field to a propagating crack surface. In cases where a residual stress is present, irregular crack shapes often evolve and you could even have a situation where part of the crack front is not advancing; a BEASY analysis will highlight these effects and characterize the effect of a residual stress field on crack propagation behaviour.

Contact Loading Effects on SIFs

Predicts the effect of contact loading on crack behaviour. BEASY’s nonlinear contact algorithm automatically computes the change in position of the contacting surfaces and the resulting stress redistribution.

BEASY’s constraint based contact algorithm computes the appropriate surface contact conditions (e.g., open, closed, sliding) and enforces these conditions using an iterative solution method. Load sequencing effects can be included, when friction is present, to accurately capture the load transfer history.

Hole propping (lugs, fasteners), and edge of contact effects (fretting fatigue), are two common contact related phenomena that influence SIF solutions; BEASY provides a powerful approach to model these coupled contact-fracture applications.

Fracture Assessment Tool

BEASY Fracture Assessment Tool (FASST) can be used to quickly assess the effect of a crack on the structural integrity of a component or structure by calculating the maximum stress intensity factor for a given crack size using the predicted 3D stress at any location. The sensitivity of the stress intensity factor to the crack size at a location can also be investigated and the data viewed graphically.  Typically stress intensity factors are computed using handbook solutions for a specific loading and model geometry or by performing a crack simulation by incorporating a crack into a simulation model. For the case where parameter studies are required the BEASY Fracture Assessment Tool automates the process of investigating multiple crack locations and the impact of multiple crack sizes. In addition to accurate stress intensity factor data, BEASY FASST provides sensitivity to crack size and location, which is valuable information to the design engineer and to those responsible for manufacturing control or maintenance

Fatigue Crack Growth Criteria

The crack growth laws supported include:

  • Paris
  • Forman
  • Rhodes
  • NASGRO (2, 3, 4, 5)
  • Walker Chang
  • Vasudevan
  • Unigrow
  • Navarro (short cracks)
  • User defined tabulated da/dn

Retardation Models

Retardation models can be used with selected growth equations to represent the effect of plasticity in the model.

  • Generalised Willenborg
  • Modified Generalised Willenborg
  • Walker Chang

Crack Growth Direction Criteria

  • Maximum Principal Stress (2D only)
  • Minimum Strain Energy Density
  • Multi-axiality (Q Plane) searching
  • Mode 1 growth

Materials Database

  • NASGRO 2/3 databases (Over 360 materials are represented)
  • Ability to link to the NASGRO 4 & 5 database
  • Alternatively users can define their own material properties

Fatigue Crack Growth Results

  • Stress Intensity Factors
  • Crack and model deformation
  • Crack and model stress field
  • Crack propagation path
  • Crack growth rate

Material Properties

  • Isotropic, linear elastic for 3D and 2D crack growth simulation
  • Isotropic, linear elastic for 3D, 2D and axisymmetric for stress analysis only
  • Orthotropic and anisotropic linear elastic for 2D and 3D for stress analysis only


  • Multi axial fatigue
  • Thermal
  • Non-linear contact

Finite Element Interfaces

BEASY is tightly integrated with popular, commercial FEA systems (ABAQUS, ANSYS & NASTRAN).  Special interfaces have been developed, that use existing FE solutions sets, to create fracture models. A unique process has been developed so that the FE mesh and loading can be used directly to create a BEASY fracture model.

Sub models can even be extracted from large, global FE solution sets, to perform localized fracture mechanics; there is no need to rebuild models just to obtain an SIF solution.  These FE Interfaces work seamlessly with the BEASY fracture toolset.  Engineers can use their existing FEA software platforms but also leverage the power of a BEASY crack growth simulation.  Post-processing of the cracked part, in your particular FE software package, is fully supported.

Global – Local Fracture Modelling

The BEASY FE Interface software combines the advantage of using large scale FE model solutions with the accuracy of high fidelity local sub-models of facture critical areas. The software also provides the technology to derive residual stress fields from non-linear FEM model solutions.  These residual stress fields can then be used to drive crack growth simulations in local sub-models.

Model Cutting Tool Software

The BEASY Model Cutting Tool is designed to simplify and automate the process of dividing models into zones. This can be particularly useful when using Finite Element models to create a BEASY model or when there is need to reduce the computational time of the simulation.

When solving stress applications, the degrees of freedom can quickly increase, especially when introducing cracks into the model. This can have a major impact on the computational time of a simulation. However, this impact can be lessened by splitting the model into “zones” which can significantly decrease the computational time. This can be done manually, which can be quite a laborious process, or the “BEASY Model Cutting Tool” can be used to quickly “cut up” an existing mesh and automatically zone and re-mesh it.

The software can also be used to cut away parts of the model which are not required for the simulation.


THE BEASY Patran Interface provides users with the capability to directly build BEASY models within MSC Patran's modeling environment. FE models can also be converted to BEASY models within the PATRAN environment. Custom interfaces have been developed to support creation of BEASY models. Once the BEASY model is complete the BEASY fracture simulation tools can be used to insert cracks. The BEASY Patran Interface also supports the design of non-standard crack shapes which can later be accessed using BEASY’s Crack Library Management tool. MSC Patran users retain full access to all the features within the Patran modeling environment while building BEASY models.

Request more information on BEASY PATRAN


The BEASY ABAQUS software interface provides an integrated approach between BEASY and ABAQUS for stress, fracture and crack growth simulation. It provides the tools to leverage existing FEM models and results to fast track the development of BEASY fracture and crack growth models. The BEASY results can then be visualised within the ABAQUS CAE environment.

It also provides the technology to derive from non-linear and transient ABAQUS models residual stress fields for use in BEASY fracture or crack growth simulation models.

Request more information on BEASY ABAQUS


The BEASY ANSYS software interface provides an integrated approach between BEASY and ANSYS for stress, fracture and crack growth simulation. It provides the tools to leverage existing FEM models and results to fast track the development of BEASY fracture and crack growth models.

It also provides the technology to derive from non-linear and transient ANSYS models residual stress fields for use in BEASY fracture or crack growth simulation models.

Request more information on BEASY ANSYS


The BEASY NASTRAN software interface provides an integrated approach between BEASY and NASTRAN for stress, fracture and crack growth simulation. It provides the tools to leverage existing FEM models and results to fast track the development of BEASY fracture and crack growth models. The BEASY results can then be visualised within the NASTRAN post-processing tool via a NASTRAN op2 file.

It also provides the technology to derive from non-linear and transient NASTRAN models residual stress fields for use in BEASY fracture or crack growth simulation models. 

Request more information on BEASY NASTRAN

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