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It is a conference presentation regarding multiscale modelling to find constitutive properties
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Effect of Multiwalled Carbon Nanotubes on Mechanical and Electrical Properties of Carbon Fiber Reinforced Polymer Composites in Aircraft Structures P.K. Sahoo*, Vinod Kumar K Dr. P.K. Sahoo • Raman Research Fellow-2012-13, Univ. Stuttgart, Germany • Principal ScientistStructural Technological DivisionCSIR-National Aerospace LaboratoriesBangalore-560017, IndiaTel.: +91 80 2508 6342, 9900523444 (Mob)Email: pks@nal.res.in, sahoopradeepk1@gmail.com ADMAT 2019, Mat Def 23-25 September 2019 Courtyard by Marriott, Hyderabad, INDIA 24thSeptember 2019
Acknowledgements • Director, CSIR-NAL, Bangalore • CSIR Grant (Projectno. MLP 1808) • Colleagues of Centre for Societal Mission & Special Technologies (CSMST) of CSIR-NAL working in the project • Masters students working in the Group
INTRODUCTION • Carbon fibre reinforced polymer (CFRP) composites are extensively used in the aerospace industries for both civilian and military aircraft structural applications • MWCNTs (which have exceptional mechanical properties and electrical conductivity) in epoxy resins improves its mechanical properties and electrical conductivity.
PROBLEM STATEMENT • Investigating the effect of MWCNTs (nanoscale materials) addition in conventional CFRP on mechanical and electrical conductivity properties • To carry out parametric studies of these properties with varying weight percentage (wt. %) of MWCNTs
Fiber Volume fraction of T300/Araldite/MWCNT Composites with varying CNT wt%
CNTs Epoxy Resin Carbon Fiber Problem Formulation MWCNT Orientation through Transformation angle ‘a’ Multi-scale Micromechanics Approach for Evaluating Effective Properties of CF/CNT/epoxy nanocomposite: Aligned MWCNT Randomly in Epoxy Resin Matrix Determination of Mechanical & Electrical Properties of CNT/Epoxy composite by Eshelby Mori-Tanka’s Model Determination of Mechanical & Electrical Properties of CF/CNT/Epoxy nanocomposite by Eshelby Mori-Tanka’s Model
Problem Formulation (Contd.) Analytical (Mori-Tanaka) Method (Stiffness): The elastic stiffness tensor C∝ can be obtained by the transformation of elastic stiffness tensor CCNT and can be expressed as Where T is the transformation matrix
Problem Formulation (Contd.) Analytical (Mori-Tanaka) Method for Electrical Conductivity: The electrical conductivity tensor S∝ can be obtained by a particular transformation of electrical conductivity tensor SCNT and can be expressed as Where Q is the transformation matrix
Problem Formulation (Contd.) FEM Method: Periodic Boundary Conditions applied to RVE to Evaluate Stiffness Constants RVE Total number of nodes: 7377 Total number of elements: 6920 6240 linear hexahedral elements of type C3D8R 680 linear wedge elements of type C3D6 Reuss Model (SoM based RoM)
RESULTS & DISCUSSION Young's Modulus E1 GPa Young's Modulus E2=E3 GPa Shear Modulus G12=G13 GPa Shear Modulus G23 GPa
RESULTS & DISCUSSION (Contd.) Electrical Conductivity of Araldite /MWCNT Composites (2-phase) • Electrical conductivity = 2.00E-08 S/m • Significant improvement in electrical conductivities (About 100% increase)
RESULTS & DISCUSSION (Contd.) Tensile Modulus T300/Araldite /MWCNT Nanocomposites (3-phase)
RESULTS & DISCUSSION (Contd.) Poisson's Ratios of T300/Araldite /MWCNT Nanocomposites (3-phase)
RESULTS & DISCUSSION (Contd.) Shear Modulus T300/Araldite /MWCNT Nanocomposites (3-phase)
RESULTS & DISCUSSION (Contd.) Electrical Conductivities of T300/Araldite /MWCNT Nanocomposites (3-phase)
Concluding remarks • Multiscale materials manufacturing and simulations are exciting and pose a great challenge • Influence of CNT wt% is more significant on electrical conductivities than on mechanical properties • Improvement in mechanical properties are essential for improving structural Integrity of structure • Improvement in electrical properties are essential for improving SHM capability of structure • Aspect ratio of CNTs that depend on manufacturing process has influence on both mechanical and conductivities-to be studied further