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© 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

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Page 1: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina ApproachRobert ShermanSenior CAE Analyst, RTP Company

Page 2: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Class Summary

In this class we will present to you a reasonable approach to structural analysis of fiber reinforced injection molded designs. We will also provide some insight into important parameters in the analysis that can be utilized to improve the simulation performance of your designs.

Page 3: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Learning Objectives

At the end of this class, you will be able to: Understand the importance of anisotropic structural analysis for good design Appreciate the need for further structural research of fiber reinforced materials Implement the lamina failure approach in predicting injection molded strength Better predict the strength of any fiber reinforced injection molded part design

Page 4: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Problem: Predicting Structural Integrity

Page 5: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Designing with Fiber Reinforced Materials

Quasi-isotropic analysis no longer acceptable Everyone wants to optimize their design

Few engineers know HOW! Validation of fiber orientation

Microscopy Microtomography (Skyscan)

New fiber orientation parameters Reduced Strain Closure (RSC) model Anisotropic Rotary Diffusion (ARD) model Fiber aspect ratio

Page 6: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

How can we validate fiber orientation?

Validate orientation by micro-mechanical property predictions If orientation is right – stiffness and strength are right

Requires thickness variations and flow/cross-flow orientation Some already done for mechanical properties

Determine correlation parameters with selected materials Tensile modulus correlation validates intensity of orientation Flexural correlation validates distribution through thickness

Page 7: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Standard Test Panels

Page 8: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

RSC Factor – Slow Orientation Dynamics

Standard Tucker-Folgar model Represents orientation in fully developed steady-state flow

RSC factor introduced Orientation requires flow history to fully develop That rate may vary based on many factors

Polymer Fibrous reinforcement Reinforcement volume content Others???

Page 9: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

RSC Factor Presents an Opportunity !!!

Glass half empty (typical user’s normal attitude!) Or, glass half full ??? Utilize new parameter to improve the orientation correlation Still requires experimentation to establish

Possibly for all major polymer types (or classes) % level of reinforcement GF, CF, VLGF, VLCF

Page 10: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

What a Difference a Factor Can Make !!!

Page 11: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

WHAT DO I DO NOW !!!!!!!

Page 12: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Start with Molded Specimen Orientation Validation

Page 13: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Molded Tensile Modulus vs. RSC & Fiber AR

Page 14: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Flow Direction Modulus vs. RSC & Fiber AR (Spec. T1)

Page 15: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Flow Direction Modulus vs. RSC & Fiber AR (Spec. T5)

Page 16: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Flow Direction Modulus vs. RSC & Fiber AR (Spec. T3)

Page 17: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Flow Direction Modulus for RSC=0.25 & AR=40

Page 18: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Cross-flow Direction Modulus for RSC=0.25 & AR=40

Page 19: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

FIBSTRS API – Nanda Santhanam

Page 20: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Composite Lamina Stress Analysis – NEi NASTRAN®

Linear material model utilizes AMI modulus predictions Don’t rely on “back-calculated” resin properties Utilize low % secant modulus (0.5-1.0%) Delete panel geometry except tensile specimen of interest Apply testing boundary conditions and test load or displacement Add estimated strength allowables to material property cards Evaluate stress distributions and failure index based on different failure criteria

Page 21: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Stress Analysis – Flow Direction Specimen T5

Page 22: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Stress Analysis – Flow Direction Specimen T5; Ply #2

Page 23: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Stress Analysis – Flow Direction Specimen T5;Ply #5

Page 24: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Summary

Micro-mechanical property predictions can assist in orientation validation RSC factor has no “default” value Fiber AR may now be a useful variable with RSC implementation Composite lamina failure techniques can detect critical stress locations Implementation of “successive ply failure” and flexural simulation should help Much room for more research

Page 25: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

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Page 26: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Questions?

Bob [email protected]

Page 27: © 2011 Autodesk Failure Analysis of Fiber Reinforced Injection Moldings Using a Composite Lamina Approach Robert Sherman Senior CAE Analyst, RTP Company

© 2011 Autodesk

Autodesk, AutoCAD* [*if/when mentioned in the pertinent material, followed by an alphabetical list of all other trademarks mentioned in the material] are registered trademarks or trademarks of Autodesk, Inc., and/or its subsidiaries and/or affiliates in the USA and/or other countries. All other brand names, product names, or trademarks belong to their respective holders. Autodesk reserves the right to alter product and services offerings, and specifications and pricing at any time without notice, and is not responsible for typographical or graphical errors that may appear in this document. © 2011 Autodesk, Inc. All rights reserved.