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ME 8883/CSE 8803: Materials Informatics 
8th December 2014 
Developing Structure-Property Linkage for Glass 
Fibre Reinforced Polymer Composites 
Presented by 
Geet Lahoti, 2nd Year ISyE PhD Student 
Alicia White, 2nd Year MSE PhD Student 
Guided by 
Prof. Surya Kalidindi 
Dr. Tony Fast
12/8/2014 2 
Background 
• Combine properties of the two materials 
Figure 1: Components of a BMW sedan fabricated with 
lignocellulosic fiber reinforced polymer (FRP) 
composites [1] Figure 2: FRP materials in passenger 
aircraft [2] 
• Composites are used in many industries 
Figure 3: Indian glass fibre composites 
market (2006) [3]
12/8/2014 3 
Background 
• Forming processes create varied 
and complex microstructures 
• Microstructure varies even within a 
simple part such as this plate 
• Understanding the complexity of 
these microstructures is an open 
field which can give insight to the 
properties of these materials 
Figure 4: Variety in microstructure across an injected part
12/8/2014 4 
Motivation 
• The structure and organization of the 
reinforcement greatly affect the final 
properties of the part 
• Conventional approaches to property 
determination do not take into account 
the microstructure of the reinforcement 
• Voigt model [4] 
• Ruess Model [5] 
• Those that do are based on a assumed 
configurations of the fibres, not the 
actual microstructure [6] 
Figure 5: Complex microstructure of FRPC.
12/8/2014 5 
Project Outline 
• Objective: Develop Structure-Property Linkage for GFRPs 
Manufacture 
GFRP Samples 
Segmentation 
Is the no. 
of 
samples 
enough? 
Spatial 
Correlation 
Microstructure 
Simulation 
Dimensionality 
Reduction 
Perform 
Micro-computed 
tomography 
(micro-CT) 
Physical Property 
from Finite 
Element Analysis 
Physical Property 
from 
Experimental 
Testing 
Relationship 
Modelling 
Yes 
No
12/8/2014 6 
Project Execution 
Step 1: Samples and Micro-CT Data 
• Fibre: Glass 
• Polymer: Polypropylene 
• Processing: hot melt impregnation and extrusion/compression molding 
• Micro-CT Images: DICOM Format 
• No. of Samples: 2 
• Dimensions of each sample: 1300 X 1300 X 900 voxels 
• Dimensions under consideration: 300 X 300 X 300 voxels
12/8/2014 7 
Project Execution 
Step 2: Segmentation 
• Need to separate the fiber from the matrix to get an 
accurate representation of microstructure 
• Apply peak fitting 
algorithm to histogram 
of pixel values 
• Segmentation based 
on Gaussian 
Likelihood 
Maximization 
• Gaussian Function 
1 
푎 
f(x) = 
(푥−푏)2 
2푐2 
푒− 
where, a=height, 
b=center, c=width 
• Multi Otsu’s Method 
Original Microstructure 
Segmented Microstructure
12/8/2014 8 
Project Execution 
Step 3: Microstructure Simulation 
Fibers Elongated along Y Axis Fibers Elongated along Diagonal Fibers Elongated along X Axis 
Dimensions: 21 X 21 X 21
12/8/2014 9 
Project Execution 
Step 4: Physical Property Simulation 
• Finite Element was performed under uniaxial strain conditions 
• Property under consideration is going to be C11. 
• Stress and strain were calculated and used to find the components of the 
stiffness tensor corresponding to Ɛ1 
Stress Strain
12/8/2014 10 
Project Execution 
Step 5: 2-Point Statistics 
• 2-Point Statistics: Probability density associated with finding local states h and 
h’ at the tail and head, respectively, of a prescribed vector r randomly placed 
into the microstructure[7]
12/8/2014 11 
Project Execution 
Step 6: Dimensionality Reduction 
• 2-Point Statistics: Extremely large set 
• Low dimensional representation 
• Principal Components Analysis [7] 
• Linear transformation of high-dimensional data to a new orthogonal frame
12/8/2014 12 
Project Execution 
Step 6: Dimensionality Reduction 
• Please add description about 2-Point Stats 
PCs for Sample 1: 0.0104 0.0000 0.0000 -0.0003 -0.0001 
PCs for Sample 2: 0.0104 0.0000 0.0001 0.0002 0.0002
12/8/2014 13 
Project Execution 
Step 7: Structure-Property Linkage 
• Regression 
Property = ퟑퟑ. ퟔ +0.88 PC1 + 15.76 PC2 + 3.83 PC3 - 5.83 PC4 + 17.22 PC5 
Rsquare: 0.9638 
CV Mean Absolute Error: 0.14237 
Property Predicted by model 
for sample 1 : 33.6129 
and 
for sample 2: 33.6098 
Property Predicted by FEM simulations 
for sample 1: 4.99 
and 
for sample 2: 6.48
12/8/2014 14 
Conclusion & Future Work 
• Investigated digital representations of sample microstructures 
• Developed a S-P linkage based on simulated dataset 
• Obtain more real samples 
• Validating linkages with the segmented real microstructures 
• Carry out physical experimental testing of samples 
• Simulate a rich set of microstructures 
• Other Studies using the same protocol: Consider other composites like 
Carbon Fibre Reinforced Polymers
12/8/2014 15 
References 
1. http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1517-70762010000200006 
2. http://www.reinforcedplastics.com/view/4437/india-on-the-up/ 
3. http://essaywritingserviceuk.co.uk/advice-and-guidance/free-essays/the-potential-of-frp-materials- 
in-a-passenger-aircraft-structure/ 
4. W. Voigt, ”On the relation between the elasticity constants of isotropic bodies," Ann 
Phys Chem 274 (1889): 573-587. 
5. A. Reuss and Z. Angrew, ”A calculation of bulk modulus of polycrystaliine materials." 
ZAMM- Journal of Apllied Mathmatics and Mechanics, Vol. 9, No. 1, 1929, pp.49-58 
6. http://onlinelibrary.wiley.com/doi/10.1002/pc.20002/pdf 
7. Surya R. Kalidindi, “Data Science and Cyberinfrastructure: Critical Enablers for 
Accelerated Development of Hierarchical Materials
12/8/2014 16 
Thank You! 
Questions?

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Final ppt v3

  • 1. ME 8883/CSE 8803: Materials Informatics 8th December 2014 Developing Structure-Property Linkage for Glass Fibre Reinforced Polymer Composites Presented by Geet Lahoti, 2nd Year ISyE PhD Student Alicia White, 2nd Year MSE PhD Student Guided by Prof. Surya Kalidindi Dr. Tony Fast
  • 2. 12/8/2014 2 Background • Combine properties of the two materials Figure 1: Components of a BMW sedan fabricated with lignocellulosic fiber reinforced polymer (FRP) composites [1] Figure 2: FRP materials in passenger aircraft [2] • Composites are used in many industries Figure 3: Indian glass fibre composites market (2006) [3]
  • 3. 12/8/2014 3 Background • Forming processes create varied and complex microstructures • Microstructure varies even within a simple part such as this plate • Understanding the complexity of these microstructures is an open field which can give insight to the properties of these materials Figure 4: Variety in microstructure across an injected part
  • 4. 12/8/2014 4 Motivation • The structure and organization of the reinforcement greatly affect the final properties of the part • Conventional approaches to property determination do not take into account the microstructure of the reinforcement • Voigt model [4] • Ruess Model [5] • Those that do are based on a assumed configurations of the fibres, not the actual microstructure [6] Figure 5: Complex microstructure of FRPC.
  • 5. 12/8/2014 5 Project Outline • Objective: Develop Structure-Property Linkage for GFRPs Manufacture GFRP Samples Segmentation Is the no. of samples enough? Spatial Correlation Microstructure Simulation Dimensionality Reduction Perform Micro-computed tomography (micro-CT) Physical Property from Finite Element Analysis Physical Property from Experimental Testing Relationship Modelling Yes No
  • 6. 12/8/2014 6 Project Execution Step 1: Samples and Micro-CT Data • Fibre: Glass • Polymer: Polypropylene • Processing: hot melt impregnation and extrusion/compression molding • Micro-CT Images: DICOM Format • No. of Samples: 2 • Dimensions of each sample: 1300 X 1300 X 900 voxels • Dimensions under consideration: 300 X 300 X 300 voxels
  • 7. 12/8/2014 7 Project Execution Step 2: Segmentation • Need to separate the fiber from the matrix to get an accurate representation of microstructure • Apply peak fitting algorithm to histogram of pixel values • Segmentation based on Gaussian Likelihood Maximization • Gaussian Function 1 푎 f(x) = (푥−푏)2 2푐2 푒− where, a=height, b=center, c=width • Multi Otsu’s Method Original Microstructure Segmented Microstructure
  • 8. 12/8/2014 8 Project Execution Step 3: Microstructure Simulation Fibers Elongated along Y Axis Fibers Elongated along Diagonal Fibers Elongated along X Axis Dimensions: 21 X 21 X 21
  • 9. 12/8/2014 9 Project Execution Step 4: Physical Property Simulation • Finite Element was performed under uniaxial strain conditions • Property under consideration is going to be C11. • Stress and strain were calculated and used to find the components of the stiffness tensor corresponding to Ɛ1 Stress Strain
  • 10. 12/8/2014 10 Project Execution Step 5: 2-Point Statistics • 2-Point Statistics: Probability density associated with finding local states h and h’ at the tail and head, respectively, of a prescribed vector r randomly placed into the microstructure[7]
  • 11. 12/8/2014 11 Project Execution Step 6: Dimensionality Reduction • 2-Point Statistics: Extremely large set • Low dimensional representation • Principal Components Analysis [7] • Linear transformation of high-dimensional data to a new orthogonal frame
  • 12. 12/8/2014 12 Project Execution Step 6: Dimensionality Reduction • Please add description about 2-Point Stats PCs for Sample 1: 0.0104 0.0000 0.0000 -0.0003 -0.0001 PCs for Sample 2: 0.0104 0.0000 0.0001 0.0002 0.0002
  • 13. 12/8/2014 13 Project Execution Step 7: Structure-Property Linkage • Regression Property = ퟑퟑ. ퟔ +0.88 PC1 + 15.76 PC2 + 3.83 PC3 - 5.83 PC4 + 17.22 PC5 Rsquare: 0.9638 CV Mean Absolute Error: 0.14237 Property Predicted by model for sample 1 : 33.6129 and for sample 2: 33.6098 Property Predicted by FEM simulations for sample 1: 4.99 and for sample 2: 6.48
  • 14. 12/8/2014 14 Conclusion & Future Work • Investigated digital representations of sample microstructures • Developed a S-P linkage based on simulated dataset • Obtain more real samples • Validating linkages with the segmented real microstructures • Carry out physical experimental testing of samples • Simulate a rich set of microstructures • Other Studies using the same protocol: Consider other composites like Carbon Fibre Reinforced Polymers
  • 15. 12/8/2014 15 References 1. http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1517-70762010000200006 2. http://www.reinforcedplastics.com/view/4437/india-on-the-up/ 3. http://essaywritingserviceuk.co.uk/advice-and-guidance/free-essays/the-potential-of-frp-materials- in-a-passenger-aircraft-structure/ 4. W. Voigt, ”On the relation between the elasticity constants of isotropic bodies," Ann Phys Chem 274 (1889): 573-587. 5. A. Reuss and Z. Angrew, ”A calculation of bulk modulus of polycrystaliine materials." ZAMM- Journal of Apllied Mathmatics and Mechanics, Vol. 9, No. 1, 1929, pp.49-58 6. http://onlinelibrary.wiley.com/doi/10.1002/pc.20002/pdf 7. Surya R. Kalidindi, “Data Science and Cyberinfrastructure: Critical Enablers for Accelerated Development of Hierarchical Materials
  • 16. 12/8/2014 16 Thank You! Questions?

Notas del editor

  1. Composites are 2 component materials that are used to combine the properties of the two materials. Our composites are made of polypropylene reinforced with glass fibers. Combining these materials increases the strength of the material while maintaining light weight and mold ability. As a result, these materials are used in many industries to create light weight parts. The ability to predict the properties of the useful materials allows rapid development of such parts.
  2. A complication to being able to predict the properties of composites is the rich variety of microstructures. Even within a simple part, there is variation of the microstructure caused by the forming methods. This image show in a location near the injection location, the fibers are highly disordered, whereas farther away the fibers have aligned to a greater degree.
  3. Conventional approaches for? What do you mean by theoretical representation? Could you please add at least one theoretical model with reference? Add figure description The structure and organization of the reinforcement greatly affect the final properties of the part. As an example, the response of a part with aligned fibers will be very different if strain is applied in the fiber direction and perpendicular to it. Many often used approaches for determining the bulk properties are based solely on volume fraction. For example, the voigt and Ruess models are used to determine bounds on what the mechanical properties can be. However, to get more accurate predictions, more knowledge of the actual structure is necessary. Other researchers have attempted to look at similar systems by using distributions of characteristics. For example one study on natural fibers as reinforcement used probability density function for the fiber lengths and diameters. T
  4. * Let me know if something doesn’t make sense. Real Microstructures Segmentation/Digitization Simulated Microstructures and Property Data Spatial Correlation (2-point Statistics) Dimensionality Reduction (PCA) Regression Model Nice chart
  5. DICOM: Digital Imaging and Communications in Medicine
  6. Simple thresholding doesn’t work since the modes of histogram are not clearly distinguishable! Otsu: maximizing the between-class variance! Gaussian Likelihood Maximization is something we made up explain it.
  7. What variety do we have within each sample type? Fiber length, volume fraction? Within what range?
  8. Please correct this slide. Add suitable values from the property you calculated. This figures are corresponding to Elongated Fibers (along X). If they doesn’t make sense let me know asap. In order to simulate the properties of the composite, finite element analysis was performed under uniaxial strain conditions. From the results, the first components of the stiffness tensor were calculated. For each sample C11 was used as a material property for use in creating the linkages.
  9. Two point statistics is a method of capturing the microstructure information in a statistical way. This is an auto correlation so measuring the likelihood that fiber is at both ends of a vector of a certain length. Directionality can be seen in the two elongated samples. The diagonal sample requires partitioning the 3D data in at an angle for visualization. The maximum values also show the volume fractions.
  10. In this project we have taken two microstructures generated from micro-CT data. We have investigated ways of using those microstructures to predict properties of the composite material. To validate this process we have used generated microstructures to create linkages between the structure of the sample and the properties. Future work on this project will include: continued investigation into the physical samples and use the results of that investigation to improve and validate the linkages we created. Other materials systems can then be investigated using this same protocol.
  11. Why ref 4 and 5 are in German?? Reference no. 6 doesn’t work. Check the link. Fixed