Auxetic Research

References (Some helpful references for Auxetic Materials)

Adams, D. F., & Miller, A. K. (1975). An analysis of the impact behavior of hybrid composite materials. Materials Science and Engineering, 19(2), 245-260.

Ahn, K. J., & Seferis, J. C. (1993). Prepreg processing science and engineering. Polymer Engineering & Science, 33(18), 1177-1188.

Alderson, K. L., Alderson, A., Smart, G., Simkins, V., & Davies, P. (2002). Auxetic polypropylene fibres. part 1. manufacture and characterisation. Plastics, Rubbers and Composites, 31(8), 344-349.

Alderson, A. (2011). Auxetic materials: Stretching the imagination. Chemistry and Industry (London), (2)

Alderson, A., Alderson, K., & Skertchly, D. (2006). Auxetic composites expand when they are stretched. JEC Composites Magazine, 43(28), 65.

Alderson, A., & Alderson, K. L. (2007). Auxetic materials. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 221(4), 565-575.

Alderson, A., Alderson, K. L., Davies, P. J., & Smart, G. M. (2005). The effects of processing on the topology and mechanical properties of negative poisson's ratio foams. 2005 ASME International Mechanical Engineering Congress and Exposition, IMECE 2005, Orlando, FL. , 70 AD. pp. 503-510.

Alderson, K. L., Alderson, A., Davies, P. J., Smart, G., Ravirala, N., & Simkins, G. (2007). The effect of processing parameters on the mechanical properties of auxetic polymeric fibers. Journal of Materials Science, 42(19), 7991-8000.

Alderson, K. L., Alderson, A., & Wojciechowski, K. W. (2011). Auxetic materials and related systems. Physica Status Solidi (B) Basic Research, 248(1), 28-29.

Alderson, K. L., & Coenen, V. L. (2008). The low velocity impact response of auxetic carbon fibre laminates. Physica Status Solidi (B) Basic Research, 245(3), 489-496.

Alderson, K. L., Pickles, A. P., Neale, P. J., & Evans, K. E. (1994). Auxetic polyethylene: The effect of a negative poisson's ratio on hardness. Acta Metallurgica Et Materialia, 42(7), 2261-2266.

Alderson, K. L., Simkins, V. R., Coenen, V. L., Davies, P. J., Alderson, A., & Evans, K. E. (2005). How to make auxetic fibre reinforced composites. Physica Status Solidi (B) Basic Research, 242(3), 509-518.

Al-Khalil, M. F. S., & Soden, P. D. (1994). Theoretical through-thickness elastic constants for filament-wound tubes. International Journal of Mechanical Sciences,36(1), 49-62.

Allegri, G., Jones, M. I., Wisnom, M. R., & Hallett, S. R. (2011). A new semi-empirical model for stress ratio effect on mode II fatigue delamination growth.Composites Part A: Applied Science and Manufacturing, 42(7), 733-740.

Allix, O., & Ladevèze, P. (1992). Interlaminar interface modelling for the prediction of delamination. Composite Structures, 22(4), 235-242.

Amara, K., Tounsi, A., Megueni, A., & Adda-Bedia, E. A. (2006). Effect of transverse cracks on the mechanical properties of angle-ply composites laminates.Theoretical and Applied Fracture Mechanics, 45(1), 72-78.

Anderson, T., & Madenci, E. (2000). Experimental investigation of low-velocity impact characteristics of sandwich composites. Composite Structures, 50(3), 239-247.

Andersons, J., Joffe, R., & Spārniņš, E. (2008). Statistical model of the transverse ply cracking in cross-ply laminates by strength and fracture toughness based failure criteria. Engineering Fracture Mechanics, 75(9), 2651-2665.

Andreas P., C. (2001). Impact dynamics and damage in composite structures. Composite Structures, 52(2), 181-188.

Angelidis, N., & Irving, P. E. (2007). Detection of impact damage in CFRP laminates by means of electrical potential techniques. Composites Science and Technology,67(3-4), 594-604.

Arumugam, V., Shankar, R. N., Sridhar, B. T. N., & Stanley, A. J. (2010). Ultimate strength prediction of Carbon/Epoxy tensile specimens from acoustic emission data. Journal of Materials Science & Technology, 26(8), 725-729.

Aslan, Z., Karakuzu, R., & Okutan, B. (2003). The response of laminated composite plates under low-velocity impact loading. Composite Structures, 59(1), 119-127.

B D Caddock and, K. E. E. (1989). Microporous materials with negative poisson's ratios. I. microstructure and mechanical properties [Abstract]. Journal of Physics D: Applied Physics, 22(12) 1877. 

A microporous, anisotropic form of expanded polytetrafluoroethylene has been found to have a large negative major Poisson's ratio. The value of Poisson's ratio varies with tensile strain and can attain values as large as -12. The microporous structure of the material is described and the mechanisms that lead to this large negative Poisson's ratio are identified. Micro-rotational degrees of freedom are observed, suggesting that a micropolar elasticity theory may be required to describe the mechanical properties.

Ballato, A. (2010). Poisson's ratios of auxetic and other technological materials. IEEE Transactions on Ultrasonics, Ferroelectrics, and Frequency Control, 57(1), 7-15.

Barbero, E. J., Sgambitterra, G., Adumitroaie, A., & Martinez, X. (2011). A discrete constitutive model for transverse and shear damage of symmetric laminates with arbitrary stacking sequence. Composite Structures, 93(2), 1021-1030.

Baughman, R. H. (2003). Auxetic materials: Avoiding the shrink. Nature, 425(6959), 667.

Benjeddou, O., Ouezdou, M. B., & Bedday, A. (2007). Damaged RC beams repaired by bonding of CFRP laminates. Construction and Building Materials, 21(6), 1301-1310.

Berthelot, J. (1999). Composite materials. Mechanical behviour and structural analysis (XXV ed., pp. 28-39) Springer.

Bertin, M., Touchard, F., & Lafarie-Frenot, M. (2010). Experimental study of the stacking sequence effect on polymer/composite multi-layers submitted to thermomechanical cyclic loadings. International Journal of Hydrogen Energy, 35(20), 11397-11404.

Bezazi, A., Boukharouba, W., & Scarpa, F. (2009). Mechanical properties of auxetic carbon/epoxy composites: Static and cyclic fatigue behaviour. Physica Status Solidi (b), 246(9), 2102-2110.

Bezazi, A., Remillat, C., Innocenti, P., & Scarpa, F. (2008). In-plane mechanical and thermal conductivity properties of a rectangular–hexagonal honeycomb structure. Composite Structures, 84(3), 248-255.

Bianchi, M., Scarpa, F., & Smith, C. W. (2010). Shape memory behaviour in auxetic foams: Mechanical properties. Acta Materialia, 58(3), 858-865.

Bland, P. W., & Dear, J. P. (2001). Observations on the impact behaviour of carbon-fibre reinforced polymers for the qualitative validation of models. Composites Part A: Applied Science and Manufacturing, 32(9), 1217-1227.

Blumenfeld, R. (2005). Auxetic strains—insight from iso-auxetic materials. Molecular Simulation, 31(13), 867-871.

Boal, D. H., Seifert, U., & Shillcock, J. C. (1993). Negative poisson ratio in two-dimensional networks under tension. Physical Review E, 48(6), 4274.

Borkowski, K., Kotousov, A., & Kahler, B. (2007). Effect of material properties of composite restoration on the strength of the restoration–dentine interface due to polymerization shrinkage, thermal and occlusal loading. Medical Engineering & Physics, 29(6), 671-676.

Caddock, B. D., & Evans, K. E. (1995). Negative poisson ratios and strain-dependent mechanical properties in arterial prostheses. Biomaterials, 16(14), 1109-1115.

Cairns, D. S. (1991). Simple, elasto-plastic contact law for composites. Journal of Reinforced Plastics and Composites, 10(4), 423-433.

Camanho, P. P., Dávila, C. G., Pinho, S. T., Remmers, J. J. C., Martínez, X., Oller, S., et al. (2008). Study of delamination in composites by using the Serial/Parallel mixing theory and a damage formulation. Mechanical response of composites (pp. 119-140; 140) Springer Netherlands.

Cantwell, W., Curtis, P., & Morton, J. (1983). Post-impact fatigue performance of carbon fibre laminates with non-woven and mixed-woven layers. Composites,14(3), 301-305.

Cantwell, W. J., Büsser, M., & Kausch, H. H. (1991). An analysis of the impact response of a composite beam. Composites Engineering, 1(5), 293-295, 297-307.

Cantwell, W. J., Curtis, P. T., & Morton, J. (1984). Impact and subsequent fatigue damage growth in carbon fibre laminates. International Journal of Fatigue, 6(2), 113-118.

Cantwell, W. J., Curtis, P. T., & Morton, J. (1986). An assessment of the impact performance of CFRP reinforced with high-strain carbon fibres. Composites Science and Technology, 25(2), 133-148.

Cantwell, W. J., Davies, P., & Kausch, H. H. (1990). The effect of cooling rate on deformation and fracture in IM6/PEEK composites. Composite Structures, 14(2), 151-171.

Cantwell, W. J., & Morton, J. (1985). Detection of impact damage in CFRP laminates. Composite Structures, 3(3-4), 241-257.

Cantwell, W. J., & Morton, J. (1989). Comparison of the low and high velocity impact response of cfrp. Composites, 20(6), 545-551.

Cantwell, W. J., & Morton, J. (1989). Geometrical effects in the low velocity impact response of CFRP. Composite Structures, 12(1), 39-59.

Cantwell, W. J., & Morton, J. (1989). The influence of varying projectile mass on the impact response of CFRP. Composite Structures, 13(2), 101-114.

Cantwell, W. J., & Morton, J. (1990). An assessment of the residual strength of an impact-damaged carbon fibre reinforced epoxy. Composite Structures, 14(4), 303-317.

Cantwell, W. J., & Morton, J. (1990). Impact perforation of carbon fibre reinforced plastic. Composites Science and Technology, 38(2), 119-141.

Cantwell, W. J., & Morton, J. (1991). The impact resistance of composite materials — a review. Composites, 22(5), 347-362.

Caprino, G., & Lopresto, V. (2001). On the penetration energy for fibre-reinforced plastics under low-velocity impact conditions. Composites Science and Technology, 61(1), 65-73.

Caprino, G., & Lopresto, V. (2000). The significance of indentation in the inspection of carbon fibre-reinforced plastic panels damaged by low-velocity impact.Composites Science and Technology, 60(7), 1003-1012.

Cartié, D. D. R., & Irving, P. E. (2002). Effect of resin and fibre properties on impact and compression after impact performance of CFRP. Composites Part A: Applied Science and Manufacturing, 33(4), 483-493.

Cesari, F., Dal Re, V., Minak, G., & Zucchelli, A. (2007). Damage and residual strength of laminated carbon–epoxy composite circular plates loaded at the centre.Composites Part A: Applied Science and Manufacturing, 38(4), 1163-1173.

Chambers, A. R., Mowlem, M. C., & Dokos, L. (2007). Evaluating impact damage in CFRP using fibre optic sensors. Composites Science and Technology, 67(6), 1235-1242.

Chaudhuri, J., & Jang, Q. (1988). Effect of special orientation on the fracture behavior of Graphite/Epoxy laminates. pp. 701.

Chen, A. S., Almond, D. P., & Harris, B. (2002). Impact damage growth in composites under fatigue conditions monitored by acoustography. International Journal of Fatigue, 24(2-4), 257-261.

Chen, C., Lin, C., & Chien, R. (2011). Thermally induced buckling of functionally graded hybrid composite plates. International Journal of Mechanical Sciences, 53(1), 51-58.

Chirima, G., Ravirala, N., Rawal, A., Simkins, V. R., Alderson, A., & Alderson, K. L. (2008). The effect of processing parameters on the fabrication of auxetic extruded polypropylene films. Physica Status Solidi (B) Basic Research, 245(11), 2383-2390.

Choi, H. Y., Wang, H. S., & Chang, F. (1992). Effect of laminate configuration and impactor's mass on the initial impact damage of Graphite/Epoxy composite plates due to line-loading impact

Choi, H. Y., & Chang, F. (1992). Model for predicting damage in graphite/epoxy laminated composites resulting from low-velocity point impact. Journal of Composite Materials, 26(14), 2134-2169.

Choi, H. Y., Wu, H. T., & Chang, F. (1991). A new approach toward understanding damage mechanisms and mechanics of laminated composites due to low-velocity impact: Part II—Analysis. Journal of Composite Materials, 25(8), 1012-1038.

Chotard, T. J., & Benzeggagh, M. L. (1998). On the mechanical behaviour of pultruded sections submitted to low-velocity impact. Composites Science and Technology, 58(6), 839-854.

Christoforou, A. P., & Yigit, A. S. (1998). Characterization of impact in composite plates. Composite Structures, 43(1), 15-24.

Chun, L. U., & Lam, K. Y. (1998). Dynamic response of fully-clamped laminated composite plates subjected to low-velocity impact of a mass. International Journal of Solids and Structures, 35(11), 963-979.

Clark, G. (1989). Modelling of impact damage in composite laminates. Composites, 20(3), 209-214.

Clarke, J. F., Duckett, R. A., Hine, P. J., Hutchinson, I. J., & Ward, I. M. (1994). Negative poisson's ratios in angle-ply laminates: Theory and experiment.Composites, 25(9), 863-868.

Coenen, V., Alderson, K., Myler, P., & Holmes, K. (2001). The indentation response of auxetic composite laminates. 6th Int. Conf. Deformation and Fracture of Composites, Manchester, UK.

Coenen, V. L., & Alderson, K. L. (2011). Mechanisms of failure in the static indentation resistance of auxetic carbon fibre laminates. Physica Status Solidi (b),248(1), 66-72.

Collombet, F., Lalbin, X., Bonini, J., Martin, V., & Lataillade, J. L. (1998). Damage criteria for the study of impacted composite laminates. Composites Science and Technology, 58(5), 679-686.

Collombet, F., Lalbin, X., & Lataillade, J. L. (1998). Damage prediction of laminated composites under heavy mass-low velocity impact

Corum, J. M., Battiste, R. L., & Ruggles-Wrenn, M. B. (2003). Low-energy impact effects on candidate automotive structural composites. Composites Science and Technology, 63(6), 755-769.

Cui, H., Wen, W., & Cui, H. (2009). An integrated method for predicting damage and residual tensile strength of composite laminates under low velocity impact.Computers & Structures, 87(7-8), 456-466.

Davies, G. A. O., Hitchings, D., & Wang, J. (2000). Prediction of threshold impact energy for onset of delamination in quasi-isotropic carbon/epoxy composite laminates under low-velocity impact. Composites Science and Technology, 60(1), 1-7.

Davies, G. A. O., & Olsson, R. (2004). Impact on composite structures. Aeronautical Journal, 108(1089), 541-563.

Davies, G. A. O., & Zhang, X. (1995). Impact damage prediction in carbon composite structures. International Journal of Impact Engineering, 16(1), 149-170.

de Freitas, M., & de Carvalho, R. (2006). Residual strength of a damaged laminated CFRP under compressive fatigue stresses. Composites Science and Technology,66(3-4), 373-378.

de Moura, M. F. S. F., & Marques, A. T. (2002). Prediction of low velocity impact damage in carbon–epoxy laminates. Composites Part A: Applied Science and Manufacturing, 33(3), 361-368.

Donescu, S., Chiroiu, V., & Munteanu, L. (2009). On the Young’s modulus of a auxetic composite structure. Mechanics Research Communications, 36(3), 294-301.

Donoghue, J. P., Alderson, K. L., & Evans, K. E. (2009). The fracture toughness of composite laminates with a negative poisson's ratio. Physica Status Solidi (B) Basic Research, 246(9), 2011-2017.

Dorey, G., & Davies, G. (1984). Impact and crashworthiness of composite structures. Structural Impact and Crashworthiness, 1(12), 2-24.

Dorey, G., Bishop, S. M., & Curtis, P. T. (1985). On the impact performance of carbon fibre laminates with epoxy and PEEK matrices. Composites Science and Technology, 23(3), 221-237.

Dorey, G., Sidey, G. R., & Hutchings, J. (1978). Impact properties of carbon fibre/Kevlar 49 fibre hydrid composites. Composites, 9(1), 25-32.

Dutra, R. C. L., Soares, B. G., Campos, E. A., & Silva, J. L. G. (2000). Hybrid composites based on polypropylene and carbon fiber and epoxy matrix. Polymer,41(10), 3841-3849.

E.J., B. (1992). A 3-D finite element for laminated composites with 2-D kinematic constraints. Computers & Structures, 45(2), 263-271.

Elmughrabi, A. E., Robinson, M., & Gibson, A. G. (2008). Effect of stress on the fire reaction properties of polymer composite laminates. Polymer Degradation and Stability, 93(10), 1877-1883.

Ersoy, N., Garstka, T., Potter, K., Wisnom, M. R., Porter, D., Clegg, M., et al. (2010). Development of the properties of a carbon fibre reinforced thermosetting composite through cure. Composites Part A: Applied Science and Manufacturing, 41(3), 401-409.

Evans, K. E., Nkansah, M., Hutchinson, I., & Rogers, S. (1991). Molecular network design. Nature, (124), 353.

Evans, K. E., & Alderson, A. (2000). Auxetic materials: Functional materials and structures from lateral thinking! Advanced Materials, 12(9), 617-628.

Evans, K. E., & Alderson, K. L. (2000). Auxetic materials: The positive side of being negative. Engineering Science and Education Journal, 9(4), 148-154.

Evans, K. E., Donoghue, J. P., & Alderson, K. L. (2004). The design, matching and manufacture of auxetic carbon fibre laminates. Journal of Composite Materials,38(2), 95-106.

Evans, K. E., Nkansah, M. A., & Hutchinson, I. J. (1994). Auxetic foams: Modelling negative poisson's ratios. Acta Metallurgica Et Materialia, 42(4), 1289-1294.

F Scarpa, e. a. (2009). Mechanical properties of non-reconstructed defective single-wall carbon nanotubes [Abstract]. Journal of Physics D: Applied Physics, 42(14) 142002. 

This paper describes the equivalent homogeneous uniaxial mechanical properties of defective single-wall carbon nanotubes. In particular, non-reconstructed defects that can be produced by ion or electronic irradiation have been considered. A discrete nonlinear finite-element approach based on the mechanical properties of individual carbon–carbon (C–C) bonds has been used. The individual C–C bonds in turn were simulated as beam structural elements. Extensive Monte Carlo based numerical simulation has been reported in the paper. The results show that the homogeneous elastic properties of the defective nanotubes can be qualitatively and quantitatively different from the pristine configurations. The defective nanotubes show a slight reduction in axial stiffness (Young's modulus), but large variations of Poisson's ratio outside the elastic bounds for isotropic materials, depending on the locations of the vacancies. The large fluctuations of Poisson's ratio can lead to extreme positive transversal contractions or to auxetic behaviour when the nanotubes are subjected to tensile loading.

Feraboli, P., & Kedward, K. T. (2006). A new composite structure impact performance assessment program. Composites Science and Technology, 66(10), 1336-1347.

Ferguson, R. F., Hinton, M. J., & Hiley, M. J. (1997). Determining the through-thickness properties of FRP materials. Composites Science and Technology, 58(9), 1411-1420.

Fuoss, E., Straznicky, P. V., & Poon, C. (1998). Effects of stacking sequence on the impact resistance in composite laminates — part 1: Parametric study.Composite Structures, 41(1), 67-77.

Garg, A. C. (1988). Delamination—a damage mode in composite structures. Engineering Fracture Mechanics, 29(5), 557-584.

Gigliotti, M., Wisnom, M. R., & Potter, K. D. (2003). Development of curvature during the cure of AS4/8552 [0/90] unsymmetric composite plates. Composites Science and Technology, 63(2), 187-197.

Goldsmith, W., Dharan, C. K. H., & Chang, H. (1995). Quasi-static and ballistic perforation of carbon fiber laminates. International Journal of Solids and Structures,32(1), 89-103.

Gómez-del Río, T., Zaera, R., Barbero, E., & Navarro, C. (2005). Damage in CFRPs due to low velocity impact at low temperature. Composites Part B: Engineering,36(1), 41-50.

González, E. V., Maimí, P., Camanho, P. P., Lopes, C. S., & Blanco, N. (2011). Effects of ply clustering in laminated composite plates under low-velocity impact loading. Composites Science and Technology, 71(6), 805-817.

Graham, J. F., McCague, C., Warren, O. L., & Norton, P. R. (2000). Spatially resolved nanomechanical properties of kevlar® fibers. Polymer, 41(12), 4761-4764.

Greve, L., & Pickett, A. K. (2006). Delamination testing and modelling for composite crash simulation. Composites Science and Technology, 66(6), 816-826.

Grima, J. N., Alderson, A., & Evans, K. E. (2005). Auxetic behaviour from rotating rigid units. Physica Status Solidi (b), 242(3), 561-575.

Grima, J. N., Ravirala, N., Galea, R., Ellul, B., Attard, D., Gatt, R., et al. (2011). Modelling and testing of a foldable macrostructure exhibiting auxetic behaviour.Physica Status Solidi (B) Basic Research, 248(1), 117-122.

Grima, J. N., Manicaro, E., & Attard, D. (2011). Auxetic behaviour from connected different-sized squares and rectangles. Proceedings of the Royal Society A: Mathematical, Physical and Engineering Science, 467(2126), 439-458.

Grubb, D. T., Prasad, K., & Adams, W. (1991). Small-angle X-ray diffraction of kevlar using synchrotron radiation. Polymer, 32(7), 1167-1172.

Gustin, J., Joneson, A., Mahinfalah, M., & Stone, J. (2005). Low velocity impact of combination Kevlar/carbon fiber sandwich composites. Composite Structures,69(4), 396-406.

Hadi Harkati, E., Bezazi, A., Scarpa, F., Alderson, K., & Alderson, A. (2007). Modelling the influence of the orientation and fibre reinforcement on the negative poisson's ratio in composite laminates. Physica Status Solidi (b), 244(3), 883-892.

Harkati, E. -., Azari, Z., Jodin, P., & Bezazi, A. (2007). Multilayer composite materials with non-usual poisson's ratios

Harkati, E. H., Bezazi, A., Boukharouba, W., & Scarpa, F. (2009). Influence of carbon fibre on the through-the-thickness NPR behaviour of composite laminates.Physica Status Solidi (b), 246(9), 2111-2117.

Hartary, P., & Zimmerman, L. (1997). Technology applications report No. 1)BALLISTIC MISSILE DEFENSE ORGANIZATION WASHINGTON DC.

Hartikainen, J., Hine, P., Szabó, J. S., Lindner, M., Harmia, T., Duckett, R. A., et al. (2005). Polypropylene hybrid composites reinforced with long glass fibres and particulate filler. Composites Science and Technology, 65(2), 257-267.

Hazell, P. J., & Appleby-Thomas, G. (2009). A study on the energy dissipation of several different CFRP-based targets completely penetrated by a high velocity projectile. Composite Structures, 91(1), 103-109.

Heimbs, S., Heller, S., Middendorf, P., Hähnel, F., & Weiße, J. (2009). Low velocity impact on CFRP plates with compressive preload: Test and modelling.International Journal of Impact Engineering, 36(10-11), 1182-1193.

Herakovich, C. T. (1984). Composite laminates with negative through-the-thickness poisson's ratios. Journal of Composite Materials, 18(5), 447-455.

Hine, P., Duckett, R., & Ward, I. (1997). Negative poisson's ratios in angle-ply laminates Springer Netherlands.

Hitchen, S. A., & Kemp, R. M. J. (1995). The effect of stacking sequence on impact damage in a carbon fibre/epoxy composite. Composites, 26(3), 207-214.

Hong, S., & Liu, D. (1989). On the relationship between impact energy and delamination area. Experimental Mechanics, 29(2), 115-120.

Hosur, M. V., Murthy, C. R. L., Ramamurthy, T. S., & Shet, A. (1998). Estimation of impact-induced damage in CFRR laminates through ultrasonic imaging. NDT & E International, 31(5), 359-374.

Hosur, M. V., Jain, K., Chowdhury, F., Jeelani, S., Bhat, M. R., & Murthy, C. R. L. (2007). Low-velocity impact response of carbon/epoxy laminates subjected to cold–dry and cold–moist conditioning. Composite Structures, 79(2), 300-311.

Hou, J. P., Petrinic, N., & Ruiz, C. (2001). A delamination criterion for laminated composites under low-velocity impact. Composites Science and Technology, 61(14), 2069-2074.

Hou, J. P., Petrinic, N., Ruiz, C., & Hallett, S. R. (2000). Prediction of impact damage in composite plates. Composites Science and Technology, 60(2), 273-281.

Howell, B., Prendergast, P., & Hansen, L. (1994). Examination of acoustic behavior of negative poisson's ratio materials. Applied Acoustics, 43(2), 141-148.

Hu, N., Sekine, H., Fukunaga, H., & Yao, Z. H. (1999). Impact analysis of composite laminates with multiple delaminations. International Journal of Impact Engineering, 22(6), 633-648.

Hughes, T. P., Marmier, A., & Evans, K. E. (2010). Auxetic frameworks inspired by cubic crystals. International Journal of Solids and Structures, 47(11-12), 1469-1476.

Im, K., Cha, C., Kim, S., & Yang, I. (2001). Effects of temperature on impact damages in CFRP composite laminates. Composites Part B: Engineering, 32(8), 669-682.

Innocenti, P., & Scarpa, F. (2009). Thermal conductivity properties and heat transfer analysis of multi-re-entrant auxetic honeycomb structures. Journal of Composite Materials, 43(21), 2419-2439.

Ishai, O., Garg, A., & Nelson, H. G. (1986). Hygrothermal effects on the mechanical behaviour of graphite fibre-reinforced epoxy laminates beyond initial failure.Composites, 17(1), 23-32.

Jang, B. Z., Chen, L. C., Wang, C. Z., Lin, H. T., & Zee, R. H. (1989). Impact resistance and energy absorption mechanisms in hybrid composites. Composites Science and Technology, 34(4), 305-335.

Jayanty, S., Crowe, J., & Berhan, L. (2011). Auxetic fibre networks and their composites. Physica Status Solidi (b), 248(1), 73-81.

Johnson, A. F., Pickett, A. K., & Rozycki, P. (2001). Computational methods for predicting impact damage in composite structures. Composites Science and Technology, 61(15), 2183-2192.

Jones, R., Williams, J. F., & Tay, T. E. (1987). Is fatigue testing of impact damaged laminates necessary? Composite Structures, 8(1), 1-12.

Karakuzua, R., Erbil, E., & Aktas, M. (2010). Damage prediction in glass/epoxy laminates subjected to impact loading. Indian Journal of Engineering and Materials Sciences, 17(3), 186-198.

Kelly, A., McCartney, L. N., Clegg, W. J., & Stearn, R. J. (2005). Controlling thermal expansion to obtain negative expansivity using laminated composites.Composites Science and Technology, 65(1), 47-59.

KIM, S., HSU, D., SEO, Y., & IM, K. (2009). Detection of stacking orientation error of CFRP composite laminates using ultrasound waves. Transactions of Nonferrous Metals Society of China, 19(Supplement 1), s124-s127.

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