Materials Today: Proceedings xxx (xxxx) xxx Contents lists available at ScienceDirect Materials Today: Proceedings journal homepage: www.elsevier.com/locate/matpr Modeling of multiwall carbon nanotubes reinforced natural rubber for soft robotic applications – A comprehensive presentation Elango Natarajan a, C.S. Hassan a, Ang Chun Kit a, M.S. Santhosh b, S. Ramesh c, R. Sasikumar b a Faculty of Engineering, UCSI University, Kuala Lumpur, Malaysia Department of Mechanical Engineering, Selvam College of Technology, Tamilnadu, India c Department of Mechanical Engineering, Presidency University, Bangalore, India b a r t i c l e i n f o Article history: Received 4 June 2020 Accepted 9 November 2020 Available online xxxx Keywords: Nonlinear material model Multiwall carbon nanotubes Mullins effect Quasi-static strain rate Component design a b s t r a c t Soft materials like rubbers, polymers and elastomers are non-linear hyper elastic materials or viscoelastic materials that show the large deformation under loading. One of the nonlinear material model is to be used in the simulation of soft mechanism. Mooney-Rivlin, Ogden, Polynomial, Arruda-Boyce, Yeoh, and Neo-Hookean and Extended Tube are some nonlinear hyperelastic material models existing in the practice. The objexctive of the current research is to present comprehensively the nonlinear material constants of the multiwall nanocarbon (MWCNT) reinforced natural rubber (NR) composites. NR/ MWCNT composites with 5%, 10%, 20% and 30% weight fractions of MWCNTs are prepared through compression molding. The uniaxial tensile test was conducted on dumb bell specimens of ASTM D412-06a standard. The respective strain–stress data from uni-axial tensile tests are further curve fitted into existing popular nonlinear hyperelastic models. The nonlinear constants of respective model are comprehensively tabulated, which designers can use in the component design and analysis. Finite element contact analysis of a cylindrical soft finger pressed against a rigid plate is conducted and presented. Ó 2020 Elsevier Ltd. All rights reserved. Selection and peer-review under responsibility of the scientific committee of the International Conference on Materials, Manufacturing and Mechanical Engineering for Sustainable Developments-2020. 1. Introduction Softmaterials like polymers, rubbers, elastomers etc. have ratedependent nonlinear elastic behaviour associated with negligible residual strain after unloading [1,2] and strain harderning, called Mullins effect. These kinds of materials are used in soft mechanism such soft robotic hand, soft actuators etc. The material properties of these materials can be greatly improved by reinforcement. The fillers in micro (106) scale or nano scale (109) may greatly increase the hardness, modulus, wear resistance, tensile strength etc of the base matrix. The reinforced composites usually will have lower density than the base matrix, but have high specific strength and specific modulus. The nature of the base matrix, filler percentage, compatibility of fillers with base matrix, aspect ratio, processing method, dispersion, distribution of fillers in the base matrix, interfacial structure and morphology are some parameters influencing the improvement of mechanical properties [3]. The composite is called nanocomposite, if nano fillers are used. The nanofillers will result the greater interface-to-volume ratio of the resultant composite. The nanofillers are in the form of nanoparticles, nanotubes, nanofibers, nanowires. Carbon nanotubes (CNTs) is one of the fillers attracted recently the researches for its extremely high modulus [4] and much stronger reinforcing effects in the polymer matrix than that shown by conventional carbon black [5,6]. They are available in the form of single wall carbon nanotubes (SWCNT), double wall carbon nanotubes (DWCNT) and multiwall carbon nanotubes (MWCNT). Blighe et al. [7] and Golshahr [8] used SWCNT and MWCNT, respectively for the reinforcement of silicone rubber Elango et al [9] investigated the effecct of MWCNT reinforcement in natural rubber and reported that there is a drastic increase in the material property by incorporating the MWCNT fillers into the polymer matrix. Prince Jaya Lal et al [10– 12] used nano silica and glass fibers to increase the material properties of the polymer composite. They reported that the increase of 42% in tensile strength and 39.46% in flexural strength was acheived with 0.75 wt% of nanosilica. Yu et al [13] used NiZn ferrite nanoparticles to reinforce polypropylene and reported that the filler acts as a nucleating agent to form beta isostatic thermoplastic https://doi.org/10.1016/j.matpr.2020.11.293 2214-7853/Ó 2020 Elsevier Ltd. All rights reserved. Selection and peer-review under responsibility of the scientific committee of the International Conference on Materials, Manufacturing and Mechanical Engineering for Sustainable Developments-2020. Please cite this article as: E. Natarajan, C.S. Hassan, A. Chun Kit et al., Modeling of multiwall carbon nanotubes reinforced natural rubber for soft robotic applications – A comprehensive presentation, Materials Today: Proceedings, https://doi.org/10.1016/j.matpr.2020.11.293 E. Natarajan, C.S. Hassan, A. Chun Kit et al. Materials Today: Proceedings xxx (xxxx) xxx and accelerators were added to NR mixer and the mastication was continued for about 20 more minutes to open up the filler aggregates in order to achieve a good NR-filler interface. The masticated nano composite was then placed into the mould and compression moulded at 160 °C for about 20 min for the vulcanization. The vulcanized filled rubber was then cured for 4 h at 200 °C in a digital oven. The dumb bell samples of thickness 2 mm as per ASTM D412-06a standard as shown in Fig. 2 were then cut from vulcanized rubber composites. It is obvious that hyper elastic materials result corresponding to the readjustment of molecular chains. The readjustment of molecular chains is due to various relaxation processes like rearrangement, reorientation, uncoiling. The material do not get sufficient time for all relaxation processes, if high rate of load is applied, and thus the material properties will be affected due to incomplete rearrangement of chains. Considering this factor, the uniaxial tensile tests were conducted at quasi static strain rate of 250 mm/ minute in InstronÒ 3366 universal tensile testing machine. The samples were marked with equidistant of 33 mm from the center of the sample and attached to the pneumatic gripper. The tensile load was gradually increased until the specimen breaks. The elongation of the sample was measured by extensometer attached to the machine. The recorded strain–stress data was further used to evaluate the nonlinear material constants as discussed in the next section. composite. Though there are many research articles in the reinforcement of polymers, we restrict our literaure as it is not our focus. The modelling of the component made of a soft material is a challenging one for design engineers. Elastomers, polymers and rubbers are assumed to be isotropic and incompressible materials. The inelastic response of the materials are neglected and only the nonlinear elastic response is considered in the modelling. In a finite strain theory, a scalar strain energy density function (W) defines the hyperelastic model of the material. The strain energy potential is represented either as a function of strain invariants W (I1, I2, I3) or a direct function of the principal stretch ratios W (k1,k2,k3). Mooney-Rivlin [14], Ogden [15,16], Arruda-Boyce [17], Yeoh [18], Polynomial [19] and Extended Tube [20,21] are some popular non-linear hyper elastic models. These models have been used in the past for modelling elastomers, rubbers, foams, polymers and biological tissues [9,22–34]. The accuracy of the prediction of the failure of a component depends on the choice of the material model and the reliability of input data into the model. It is more important for any design engineer to appropriately choose the material model that characterizes the behaviour of material. The stability of the material model and quality of fitting of the experimental strain–stress data are other factors to be considered in the selection of the model. The aim of this research is to synthesize the NR/MWCNT composites with different filler fractions and to evaluate nonlinear material constants of the composites. The presented material constants can be used in structural analysis of any component of these materials. 3. Hyperelastic material models and numerical simulation Hyperelastic constitutive models are grouped into three; phenomenological models, response type models, and micromechanical models. In phenomenological models, the macro mechanics of deformation of the material is used to derive the constitutive equation. In response type models, the Invariants and stretch ratios of hyperelastic strain energy potentials are directly determined from the experimental data. In micromechanical models, stochastic kinetics of deforming polymer chains are considered for the modeling. They evaluate the strainenergy potentials based on the micromechanical deformation of the material. The strain invariants I1, I2, I3 are used in Mooney-Rivlin, Polynomial, Arruda-Boyce and Yeoh models to represent the strain energy density function W. The principal stretch ratios k1, k2, k3 are used in Ogden model to represent strain energy density function. All these models are available in commerical finite element (FE) software. The substitution of experimentally measured data into the strain energy function of the respective model will result the material constants. The general form of Mooney-Rivlin model is 2. Sample preparation and experimentation MWCNT, NANOCYLÒ NC7000TM series, was supplied by Nanocyl, Belgium. RMA 1 natural rubber was supplied by Aerospace Engineers Pvt. Ltd. RMA 1 rubber is pure in composition, light in colour, acid, salt and alkaline resistant material that make it to be used in many industrial applications including tyres. MWCNTs are thin tube shaped materials produced by the supplier through the Catalytic Chemical Vapour Deposition (CCVD) process. The average diameter, length and density of the tube are 9.5 nm, 100 mm and 1.3 g/cm3 respectively. 5%, 10%, 20% and 30% of MWCNTs were considered in the preparation. Fig. 1 shows the TEM image of MWCNT used and Table 1 shows the weight fractions of the materials used in synthesing the nano composites. RMA 1 and ingredients mentioned in Table 1 were initially mixed together in two roll mill for about 20 min. The predetermined quantity of MWCNTs i j k W ðI1 ; I2 ; I3 Þ ¼ R1 i;j;k¼0 C i;j;k ðI 1 3Þ ðI2 3Þ ðI3 1Þ ð1Þ where, Ci,j,k are material constants. The shear modulus and bulk modulus of the material can be estimated from Mooney-Rivlin constants as Go ¼ 2ðC 10 þ C 01 Þ Ko ¼ 2 d ð2Þ ð3Þ The parameter d allows for the inclusion of compressibility, it is assumed to be zero for incompressible materials. If uniaxial tensile test data are used for modeling, the parameter d can be estimated as; d ¼ 1=500Go ð4Þ The poison’s ratio and linear elastic modulus of the material can be estimated as; Fig. 1. TEM image of NC7000TM MWCNT – scale: 100 nm (from the supplier). 2 Materials Today: Proceedings xxx (xxxx) xxx E. Natarajan, C.S. Hassan, A. Chun Kit et al. Table 1 Materials used and their weight fractions. Description 1 2 3 4 RMA 1 natural rubber (47 Shore A) NC7000TM MWCNT (weight fraction) Length = 1.5 mm, diameter = 9.5 nm, density = 1.3 g/cc. 95 5 90 10 80 20 70 30 Other ingredients and accelerators 4020 – 0.0016%, TDQ – 0.0015, Zinc oxide – 0.005%, Stearic acid – 0.002%, TMT – 0.0026%, CBS – 0.001%, Sulphur (accelerator) – 0.001% v¼ 3K 0 2G0 6K 0 þ 2G0 ð5Þ Eo ¼ 6ðC 10 þ C 01 Þ ð6Þ The general form of Ogden model is h i W ðk1 ; k2 ; k3 Þ ¼ Rni¼1 lai k1 ai þ k2 ai þ k3 ai 3 Fig. 2. Dumb bell specimen as per ASTM D412-06a standard. i Fig. 3. Curve fit of NR/5% MWCNT data into a) Mooney-Rivlin b) Ogden c) Neo-Hookean d) Yeoh e) Polynomial f) Arruda-Boyce models. 3 ð7Þ E. Natarajan, C.S. Hassan, A. Chun Kit et al. Materials Today: Proceedings xxx (xxxx) xxx Eq. (1) can also be redefined in terms of first two invariants as, 3 ð8Þ I2 ¼ ka12 þ ka22 þ ka32 3 ð9Þ a1 a1 a1 I1 ¼ k1 þ k2 þ k3 This is model is generalized form of Rivlin model. The extended-tube model is a physics-based polymer model, that uses the strain-energy potential. The general form of Extended tube model is W¼ m and k of Ogden model are shear modulus and limiting network stretch respectively. The linear elastic modulus of the material can be estimated from Ogden constants as: Eo ¼ 2G0 ð1 þ v Þ ¼ ð10Þ The general form of Yeoh model is W ¼R n i¼1 C i ðI1 3Þ i ð11Þ n I;J¼0 # 2Ge 2 þ In 1 d ð ð I 3 Þ Þ þ 2 1 b 1 d2 ðI1 3Þ 3 X 1 2 kb i 1 þ ðJ 1Þ d There are 5 material constants involved in this strain energy function. Gc represents crosslinked network modulus, Ge represents constraint network modulus, b is empirical parameter ð0 6 b 6 1Þ; d, and d are extensibility and incompressibility parameters respectively. b is physically derived for a given polymer network as a function of the amount of solvent, solution fraction, network defects and filler. The model may also be chosen based on the elongation of the material. In general, Neo-Hookean model is used for the material that elongates upto 30%. Mooney-Rivlin is used when the elongation is in the range of 30–200%. Arruda-Boyce model, Polynomial model and Yeoh model are suitable for elongation upto 300%. Ogden model is better model for the material having elongation upto 700%. The uniaxial stress–strain data or volumetric data of the material are measured from uni-axial or bi-axial test or shear test as per ASTM standard. The user can use any one of the test data or multiple test data for the modeling. The experimental data are curve fitted into respective hyperelastic material model to obtain the material constants. Mooney model presents two parameters, three parameters, 5 parameters, and 9 parameters material con- ð12Þ where n is number of chain segments, kB is Boltzmann constant, h is temperature in Kelvin, N is number of chains in network of crosslinked polymer. This model is based on the statistical mechanics of material with cubic representative volume element containing eight chain along the diagonal direction. The polynomial hyperelastic model is formulated in terms of the two strain invariants I1 and I2 of the Cauchy-Green deformation tensor. The strain energy function is W ðI1 ; I2 Þ ¼ R C i;j ðI1 3Þi ðI2 3Þj " 1 d2 ðI1 3Þ i¼1 where, Ci are material constants, 2C1 is the initial shear modulus of the material. When n = 1, Yeoh model reduces to Neo-Hookean model. The general form of Arruda-Boyce model is pffiffiffi pffiffiffi sinhb W ¼ NkB h n bkchain nln b Gc 2 ð13Þ Fig. 4. Curve fit of NR/10% MWCNT data into a) Mooney-Rivlin b) Ogden c) Neo-Hookean d) Yeoh e) Polynomial f) Arruda-Boyce models. 4 Materials Today: Proceedings xxx (xxxx) xxx E. Natarajan, C.S. Hassan, A. Chun Kit et al. Fig. 5. Curve fit of NR/20% MWCNT data into a) Mooney-Rivlin b) Ogden c) Neo-Hookean d) Yeoh e) Polynomial f) Arruda-Boyce models. norm/residual values is considered as the better curve fit of the model. It helps the user to assess the result whether to accept the results. The another better way to assess the curve fit is Visual fit mode in which the user can visually see the curve fit of experimental data and decide whether the results are acceptable. If the results are not acceptable, the user can choose the higher order, or increase the iterations and repeat the curve fitting. Figs. 3–6 depict curve fit of experimentally measured data into various models. The quality of the curve fit was visually noticed in all the models in all cases of the composites, which regarded the accuracy of the results. Moreover the error norm/residual values obtained from all simulations was less than 50 which confirms the quality of the curve fit of the models alternatively. The nonlinear material constants of NR composites of different weight fractions are presented in Tables 2 and 3. The design engineers can use one of the models of his own choice in their analysis. stants. Ogden model presents the constants with 1st order, 2nd order and 3rd order. It adopts Levenberg-Marquardi nonlinear least squares optimization algorithm to determine material constants of Ogden’s stress deformation function. In general, the material property is more accurately represented by higher order models. Finite element analysis (FEA) software such as ANSYS, Marc, COMSOL, ABACUS provide the curve fit modules and options to curve fit the strain–stress data to derive the material constants of different nonlinear models. The curve fitting process is based upon the regression analysis using least sqaure method. The material constants can be found from the experimental strain–stress data and constitutive equation for the principal true stress r11 under uniaxial. The quality of the fitting is mostly assessed by comparing visually the curves obtained with hyperelastic models to the experimental data. The experimentally measured strain–stress data of NR/ MWCNTs composite of different filler fractions were applied to Mooney-Rivlin (3 parameters), Ogden (3rd order), Polynomial, Yeoh, and Arruda-Boyce models through curve fitting. ANSYS provides options to curve fit nonlinear hyperleastic models and viscoelastic models. Three control parameters of the nonlinear regression model are number of iterations, residual tolerance and coefficient change tolerance. The solution stops when both the residual tolerance and the coefficient change tolerance of the erron norm are met, or the number of iterations is met. For the current analyses, the number of iterations was set to 1000 and normalized least square fit option was chosen. Visual fit and the error norm/residual values are two factors through which the acceptability of the results are determined. When the curve fit plot is printed on the screen, the error norm/ residual values is also printed on the GUI window. The smaller error 4. Case study The purpose of this case study is to show the application of nonlinear model in FE analysis. In the past, Elango et al [26] developed a contact model for power grasping using soft finger. They attempted with Silicone, Viton, Neoprene elastomeric materials. The power grasping is a type of grasping in which many contact points will be used for grasping the object. The numerical study is required for grasp manipulations before authors take up the path planning. Fig. 7 shows the contact model of the cylindrical soft finger pressed against a rigid body as power grasping, in which the deformation of the finger (d0) and contact width (w) are measured against the normal force (F). 5 E. Natarajan, C.S. Hassan, A. Chun Kit et al. Materials Today: Proceedings xxx (xxxx) xxx Fig. 6. Curve fit of NR/30% MWCNT data into a) Mooney-Rivlin b) Ogden c) Neo-Hookean d) Yeoh e) Polynomial f) Arruda-Boyce models. Table 2 Nonlinear constants of Mooney-Rivlin, Neo-Hookean, Yeoh and Arruda-Boyce models. Filler % 5% 10% 20% 30% Mooney-Rivlin (3 parameters) model Neo-Hookean model Yeoh model C10 C01 C11 m C10 C20 m Arrda-Boyce model k 1.096958 1.416277 0.864849 2.11687 1.03862 0.357 2.487001 7.965075 0.03872 0.04437 0.088338 0.58387 0.813225 2.221848 4.61169 7.043666 0.345177 1.140026 2.53247 3.583066 0.002238 0.00506 0.02545 0.0095 0.706919 2.221848 4.61169 7.043666 5.45516 81,681,725 67,985,149 23,248,482 Table 3 Nonlinear constants of Ogden and polynomial models. Filler % 5% 10% 20% 30% Ogden (3rd order) model Polynomial model m1 a1 m2 a2 m3 a3 C10 C01 0.171536 0.794482 0.623713 0.170897 2.358751 1.919898 3.118536 4.701839 0.171536 0.794482 20.41128 21.32771 2.358751 1.919898 0.251752 0.390028 0.171536 0.794482 20.52394 21.36175 2.358751 1.919898 0.249966 0.404207 0.554358 1.074612 1.692903 2.83703 0.3798 0.069335 1.370455 1.390453 b) When the load is applied over the top, the deformation of the soft finger is uniform through out the length, and hence, 2D FE model was rendered and analysis was done accordingly. c) Due to the symmetry of the problem, only quarter of the cylindrical finger was modelled and plane strain condition was applied for the analysis. d) The rigid plate was considered to be made of mild steel with modulus of elasticity E = 2.05 105 N/mm2 and poison’s ratio t = 0.3. Due to the symmetry of the geometry, only a quarter of the finger was considered in the current nonlinear contact analysis. The FE model was developed in ANSYS 18.0 with the following considerations; a) The solid cylinder of diameter 17.8 mm, made of NR/20% MWCNT material was considered for the current analysis. The material is a homogeneous, incompressible, nonlinear hyper elastic, isotropic material. Hence, the nonlinear material model, Ogden constants were used as a material model. 6 Materials Today: Proceedings xxx (xxxx) xxx E. Natarajan, C.S. Hassan, A. Chun Kit et al. has plasticity, hyper elasticity, stress stiffening, large deflection, and large strain capabilities. Fig. 8 shows the mesh model of soft cylindrical finger with 2155 nodes. The nonlinear material model with Ogden constants were selected and m1 = 0.623713, a1 = 3.118536, m2 = 20.41128, a2 = 0.251752, m3 = 20.52394, a3 = 0.249966 were input to the model. The mixed formulation was also applied in the simulation. The soft-to-hard contact pair was created between the cylinder and the plate. The constrains in x-direction were appropriately imposed along the axis of symmetry. The coupled elements on the top of the soft cylinder are expected to have uniform pressure. All directions of the rigid target surface were fixed. The load of 100 N was applied over the soft cylinder which is normal to the rigid target surface. The FE model was simulated after imposing appropriate boundary conditions stated above. The simulation was computed in 2 s in the Intel(R) Core(TM) I7-7500U CPU @ 2.70 GHz 2.90 GHz with 16 GB RAM. The deformation of the soft finger was measured at the reference node associated with the top surface. Fig. 9 shows the deformation and Von-Mises stress of the cylinder at 100 N of normal load. The maximum deformation noticed on the finger is 3.591 mm. The maximum Von-Mises stress noticed on the cylinder is 10.6633 N/mm2. The ultimate tensile strength of the NR/20% MWCNT is 14.735 MPa [9]. Since the nominal stress (r0) is less than the strength (Su) of the material, the design is regarded to be safe. Fig. 7. Contact model of a soft finger pressed against the rigid object [26]. 5. Conclusions The aim of this paper is to provide the nonlinear material constants of NR/MWCNT nano composites comprehensively to the readers and designers, which they can use in the component design and analysis. MWCNTs, filler weight fraction of 5%, 10%, 20% and 30% were mixed with RMA 1 NR matrix in two roll mill thoroughly. The masticated NR/MWCNT composites were compression moulded from which dumb bell specimens were then prepared. Uniaxial tensile tests were conducted as per ASTM ASTM D412-06 a standard and uniaxial stress–strain data of each sample was recorded. The experimental data were then applied into Mooney-Rivlin, Ogden, Neo-Hookean, Yeoh, Polynomial and Aruda-Boyce models and the respective nonlinear material constants were evaluated and tabulated for the component design and analysis. A case study-FE analysis was conducted on a cylindrical soft finger when it is pressed against a rigid mild steel plate. The simulation results show that the induced nominal stress from 100 N is within the strength of the material, which regarded the safe component design. Fig. 8. Mesh model – NR/20% MWCNT cylinder pressed against a mild steel rigid plate. e) The non-linear with large deformation condition was applied, as the material of the soft finger is a hyperelastic material. The accuracy of any FE analysis depends on the mesh elements and material model used in the analysis. Hence, they were chosen very carefully in order to get the converged results from the analysis. The non-linear hyper elastic quadrilateral elements were used to perform FE meshing. The four noded 2D Plane elements chosen Fig. 9. (a) Deformation plot (b) Von-Mises stress plot. 7 E. Natarajan, C.S. Hassan, A. Chun Kit et al. Materials Today: Proceedings xxx (xxxx) xxx [15] M. Mooney, A theory of large elastic deformation, J. Appl. Phys. 11 (9) (1940) 582–592. [16] R.W. Ogden, Large deformation isotropic elasticity - on the correlation of theory and experiment for incompressible rubber like solids, Proc. R. Soc. London 326 (1972) 398–416. [17] E.H. Twizell, R.W. Ogden, Non-linear optimization of the material constants in Ogden’s stress-deformation function for incompressinle isotropic elastic materials, J. Aust. Math. Soc. Ser. B. Appl. Math. 24 (04) (1983) 424. [18] E.M. Arruda, M.C. Boyce, A three-dimensional constitutive model for the large stretch behavior of rubber elastic materials, J. Mech. Phys. Solids 41 (2) (1993) 389–412. [19] O.H. Yeoh, Some Forms of The Strain Energy Function For Rubber, 1993, pp. 754–771. [20] R.S. Rivlin, D.W. Saunders, Large elastic deformations of isotropic materials. VII. Experiments on the deformation of rubber, Philos. Trans. R. Soc. A Math. Phys. Eng. Sci. 243 (865) (1951) 251–288. [21] M. Kaliske, G. Heinrich, An extended tube-model for rubber elasticity: statistical-mechanical theory and finite element implementation, Rubber Chem. Technol. 72 (4) (1999) 602–632. [22] R. Behnke, M. Kaliske, The extended non-affine tubemodel for crosslinked polymer networks: physical basics, implementation, and application to thermomechanical finite element analyses, in: Designing of Elastomer Nanocomposites: From Theory to Applications, K. W. Sẗockelhuber, A. Das, and M. Kl̈uppel, Eds., vol. 275 of Advances in Polymer Science, Springer, 2016, pp. 1–70. [23] M.S. Hoo Fatt, X. Ouyang, Integral-based constitutive equation for rubber at high strain rates, Int. J. Solids Struct. 44 (20) (2007) 6491–6506. [24] H. Khajehsaeid, J. Arghavani, R. Naghdabadi, S. Sohrabpour, A viscohyperelastic constitutive model for rubber-like materials: a rate-dependent relaxation time scheme, Int. J. Eng. Sci. 79 (2014) 44–58. [25] B. Song, W. Chen, M. Cheng, Novel model for uniaxial strain-rate-dependent stress-strain behavior of ethylene-propylene-diene monomer rubber in compression or tension, J. Appl. Polym. Sci. 92 (3) (2004) 1553–1558. [26] H. Khajehsaeid, J. Arghavani, R. Naghdabadi, A hyperelastic constitutive model for rubber-like materials, Eur. J. Mech. A/Solids 38 (2013) 144–151. [27] N. Elango, R. Marappan, Analysis on the fundamental deformation effect of a robot soft finger and its contact width during power grasping, Int. J. Adv. Manuf. Technol. 52 (5–8) (2011) 797–804. [28] N. Elango, A.A.M. Faudzi, A. Hassan, M.R.M. Rusydi, Experimental investigations of skin-like material and computation of its material properties, Int. J. Precis. Eng. Manuf. 15 (9) (2014) 1909–1914. [29] N. Elango, A.A. Mohd Faudzi, M.R. Muhammad Razif, I.N.A. Mohd Nordin, Determination of Non-Linear Material Constants of RTV Silicone Applied to a Soft Actuator for Robotic Applications, Key Eng. Mater., vol. 594–595, no. January 2019, pp. 1099–1104, 2013. [30] M.R.M. Razif, A.A.M. Faudzi, M. Bavandi, N.A.M. Nordin, E. Natarajan, O. Yaakob, Two chambers soft actuator realizing robotic gymnotiform swimmers fin, 2014 IEEE Int. Conf. Robot. Biomimetics, IEEE ROBIO (2014) 15–20. [31] M.S. Santhosh, R. Mohanraj, G. Karthikeyan, Mechanical and morphological behavior of rice husk/prosopis juliflora reinforced bio composites, Mater. Today:. Proc. (2019), https://doi.org/10.1016/j.matpr.2019.12.021. [32] N. Maniselvam, M.S. Santhosh, R. Sasikumar, P. Murugesan, M. Chandru, Study of corrosion behavior of carbon fiber reinforced plastics (CFRPs), Mater. Sci. Forum 969 (2019) 175–180. [33] E. Natarajan, A.A. Mohd Faudzi, V.M. Jeevanantham, M.R. Muhammad Razif, I. N.A. Mohd Nordin, Numerical Dynamic Analysis of a Single Link Soft Robot Finger, Appl. Mech. Mater., 459 (2015) 449–454. [34] M.R. Muhammad Razif, N. Elango, I.N.A. Mohd Nordin, A.A. Mohd Faudzi, NonLinear Finite Element Analysis of Biologically Inspired Robotic Fin Actuated by Soft Actuators, Appl. Mech. Mater., 528 (2017) 272–277. CRediT authorship contribution statement Elango Natarajan: Conceptualization, Methodology, Writing review & editing. C.S. Hassan: Software, Data curation. Ang Chun Kit: Writing - original draft. M.S. Santhosh: Visualization, Investigation. S. Ramesh: Supervision. R. Sasikumar: Validation. Declaration of Competing Interest The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper. References [1] J.S. Bergstrom, M.C. Boyce, Constitutive modeling of the large strain time– dependent behavior of elastomers, J. Mech. Physics. Solids 46 (1998) (1998) 931–954. [2] L.M. Yang, V.P.W. Shim, C.T. Lim, A visco-hyperelastic approach to modelling the constitutive behaviour of rubber, Int. J. Impact Eng. 24 (6–7) (2000) 545– 560. [3] N. Elango, A.A.M. Faudzi, A review article: Investigations on soft materials for soft robot manipulations, Int. J. Adv. Manuf. Technol. 80 (5–8) (2015) 1027– 1037. [4] M.M.J. Treacy, T.W. Ebbesen, J.M. Gibson, Exceptionally high Young’s modulus observed for individual carbon nanotubes, NEC Res. Inst. 382 (20) (1996) 678– 680. [5] L. Bokobza, Multiwall carbon nanotube elastomeric composites: a review, Polymer (Guildf) 48 (17) (2007) 4907–4920. [6] A.J. Crosby, J.Y. Lee, Polymer nanocomposites: the ‘nano’ effect on mechanical properties, Polym. Rev. 47 (2) (2007) 217–229. [7] V. Sathiyamoorthy, T. Sekar, N. Elango, Optimization of Processing Parameters in ECM of Die Tool Steel Using Nanofluid by Multiobjective Genetic Algorithm, Sci. World J. 2015 (2015) 1–7. [8] F.M. Blighe, W.J. Blau, J.N. Coleman, Towards tough, yet stiff, composites by filling an elastomer with single-walled nanotubes at very high loading levels, Nanotechnology, 19 (41) (2008) Article ID 415709. [9] E. Alireza Golshahr, M.S. Natarajan, R. Santhosh, S.R. Sasikumar, R. Durairaj, Multi wall carbon nanotube reinforced silicone for aerospace applications, Int. J. Mech. Prod. Eng. Res. Dev. 8 (4) (2018) 775–784. [10] N. Elango, N.S. Gupta, Y.L. Jiun, A. Golshahr, The effect of high loaded multiwall carbon nanotubes in natural rubber and their nonlinear material constants, J. Nanomater. 2017 (2017) 1–16. [11] L. Prince Jeya Lal, S. Ramesh, S. Parasuraman, E. Natarajan, I. Elamvazuthi, Compression after impact behaviour and failure analysis of nanosilicatoughened thin epoxy/gfrp composite laminates, Materials, 12 (19) (2019). [12] P.J.L. Lazar, R. Sengottuvelu, E. Natarajan, Assessments of secondary reinforcement of epoxy matrix-glass fibre composite laminates through nanosilica (SiO2), Materials 11 (11) (2018). [13] L. Prince Jeya Lal, S. Ramesh, E. Natarajan, Study on the repeatability of manufacturing nano-silica (SiO2) reinforced composite laminates, IOP Conference Series: Materials Science and Engineering, 2019. [14] L. Yu, S.H. Ahmad, I. Kong, M.A. Tarawneh, S.B.B. Abd Razak, E. Natarajan, C.K. Ang, Magnetic, thermal stability and dynamic mechanical properties of beta isotactic polypropylene/natural rubber blends reinforced by NiZn ferrite nanoparticles, Defence Tech. 15 (6) (2019) 958–963, https://doi.org/10.1016/ j.dt.2019.03.001. 8