February 6, 2012
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The Leading Software Solution for Material and Structural Failure Analysis
Quick News & Press Release
GENOA 4.4 Released
NANO Capability Introduced
New PFA Unit Cell
New MCO Unit Cell
Issue #20 - 4/13/2010
Material Characterization & Qualification (MCQ)
Issue #19 - 11/17/2009
Composite Structures & Parametric Robust Design (PRD)
Issue #18 - 7/13/2009
Numerical Approach to Determine Crack Path and Delamination Growth in Composite Structures
Issue #17 - 5/4/2009
Certification-by-Analysis (CBA)
Issue #16 - 10/20/2008
Material Qualification and Certification Determine Allowables by Means of Virtual Simulation Combined With Limited Testing
Issue #15 - 6/10/2008
Predicting Post-Buckling Response and Ultimate Failure of Composite 2-Stringer Panels
Issue #14 - 4/28/2008
Composite Storage Module Joint Analysis and Test Verification
Issue #13 - 2/25/2008
GENOA 4.3 Release with A- and B-Basis Allowables
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PFA Static
 

Progressive Failure Analysis Static (PFA_STATIC)

View Product Datasheet (PDF)

Product Highlights:

·          Predicts the maximum loads that composite and metallic elements and structures can sustain using a step-by-step virtual loading procedure that takes into consideration material degradation, nonlinearity and changes in structural geometry. Degradation of material properties is based on 1) matrix plasticity and micro-cracking; 2) fiber orientation changes and breakage; and 3) environmental effects and manufacturing defects.

·         Predicts crack initiation and growth. The program computes various damage locations and failure modes in composites caused by the application of external static loads, temperatures and environmental effects.

·         Predicts damage events at different material scales beginning with the micro-cracking in fiber, matrix and fiber/matrix interface. Damage propagation is tracked from the micro-level to ply, laminate and structural levels.

·         Optional use of conventional fracture mechanics approaches such as Virtual Crack Closure Technique (VCCT) and Discrete Cohesive Zone Model (DCZM).

·         Predicts the post-buckling response of a composite structure based on the superposition of a required scaled buckle shape on the initial geometry of the structure.

·         Predicts the time to failure as well as time-dependent crack initiation and growth in composite elements and structures caused by external static loads, temperature and environmental effects (creep response).

·         Effective for permeability and damage tolerant design of composite structures. The program computes crack density and corresponding material degradation in composite materials during the loading process.

·         Can be used as a virtual testing tool to reduce physical experimental testing by closely simulating the actual testing process.

·         Comes with its own default finite element solver MHOST.

·         Integrates numerous commercial FEM software's including: MSC.NASTRAN, MSC.MARC, ABAQUS, ANSYS and LS-DYNA. Allows the user to import, handle and run finite element models prepared for MSC.NASTRAN, MSC.MARC, ABAQUS, ANSYS and LS-DYNA.

Applications/Benefits:

·         Aerospace, automotive and construction industries.

·         Prediction/characterization of complicated failure mechanisms that can occur in aerospace and automotive composite structures.

·         Prediction of damage and fracture initiation, progression and structural collapse.

·         Determination of the ultimate strength of composite and metal structures. 

·         Determination of the residual strength of a composite structure after impact/fatigue.

·         Prediction of inspection intervals and certification requirements.


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