[1] Voigt W, Lehrbuch der Kristallphysik. B. G. Teubner-Verlag, (1928) Leipzig Berlin.

[2] Lempriere B M, AIAA J (1968), Poisson's ratio in orthotropic materials. Aiaa 6, 2226.

[3] Lakes. R (1987) Foam structures with a negative Poisson’s ratio .Science. 1987: 1038–1041.

[4] Donoghue J P, Alderson K L, and Evans K  E (2009) the fracture toughness of composite laminates with a negative Poisson's ratio. Phys. Status Solidi B 246.9: 2011 2017.

[5] Bohara R P, Linforth S, Ghazlan A, Nguyen T, Remennikov A, & Ngo T (2022) Performance of an auxetic honeycomb-core sandwich panel under close-in and far-field detonations of high explosive. Compos. Struct 280, 114907.‏

[6] Luo C, Han C Z, Zhang X Y, Zhang X G, Ren X, Xie  Y M  (2021) Design manufacturing and applications of auxetic tubular structures: A review. Thin-Walled Struct. 163 107682.

[7] Gibson L J, Ashby M F, Proc R, Soc,  Lond  A (1982), 382, 43.

[8] Gibson L J, Ashby M F, Schayer G S, Robertson C I, Proc. Roy. Soc. Lond. (1982) A, 382, 25.

[9] Gibson L J  (1981)  The elastic and plastic behaviour of cellular materials, Ph.D. Thesis, Churchill College, University of Cambridge, UK

[10] Dutta S, Menon HG, Hariprasad MP, Krishnan A, Shankar B (2020). Study of auxetic beams under bending: A finite element approach. Mater. Today

[12] Mondal P, Jayaganthan R, (2024) Theoretical and Numerical Investigation of Mechanical Properties of Auxetic S-structure under Transverse Load.

[13] Zhang C, Lu F, Wei T, Huang Y, He Y, Zhu Y. (2024) A novel windmill-shaped auxetic structure with energy absorption enhancement. Int. J. Mech. Sci. 280, 109635

[14] Yang J, Huang X-H, Shen H-S (2020). Nonlinear vibration of temperature-dependent FG-CNTRC laminated plates with negative Poisson’s ratio. Thin-Walled Struct.

[15] Gao Q, Liao W-H (2021) Energy absorption of thin walled tube filled with gradient auxetic structures-theory and simulation. Int J Mech Sci 201:106475

[16] Tran TT, Pham QH, Nguyen-Thoi T, Van TT (2020) Dynamic analysis of sandwich auxetic honeycomb plates subjected to moving oscillator load on elastic foundation. Adv Mater Sci Eng 2020:1–16.

[17] Mohandesi N, Talebitooti M, Fadaee M (2024) Mathematical modeling of free vibration of star-shaped auxetic rectangular plate. Arch. Appl. Mech.: 1-13.‏

[18] Hosseini R, Babaei M,  Naddaf Oskouei A (2023) The influences of various auxetic cores on natural frequencies and forced vibration behavior of sandwich beam fabricated by 3D printer based on third-order shear deformation theory. JCAMECH 54(2), 285-308.‏

[19] Aktas K G, Pehlivan F, Esen I (2024). Temperature-dependent thermal buckling and free vibration behavior of smart sandwich nanoplates with auxetic core and magneto-electro-elastic face layers. Mech Time-Depend Mat 1-41.‏

[20] Jiang W, Zhou J, Liu J, Zhang M, & Huang  W (2023) Free vibration behaviours of composite sandwich plates with reentrant honeycomb cores. Appl. Math. Model. 116, 547-568.‏

[21] H  Mohammadi, A  Setoodeh (2020), FSDT-based iso geometric analysis for free vibration behavior of functionally graded skew folded plates, Iran. J. Sci. Technol. Trans. Mech. Eng. 44 841-863.

[22] Javani M, Kiani Y, Eslami M R (2022) on the free vibrations of FG-GPLRC folded plates using GDQE procedure. Compos. Struct 286: 115273

[23] Thakur B R, Verma S, Singh B N, & Maiti D K (2021). Dynamic analysis of flat and folded laminated composite plates under hygrothermal environment using a nonpolynomial shear deformation theory. Compos. Struct 274, 114327.

[24] Lee S Y, Wooh S C, Yhim S S (2004) Dynamic behavior of folded composite plates analyzed by the third order plate theory, Int. J. Solids Struct. 41: 1879-1892.

[25] Zhang  J, Li  L  (2023)  Free vibration of functionally graded graphene platelets reinforced composite porous L-shaped folded plate, Eng. Struct. 297: 116977.

[26] QING T D,  ZHI C Y  (2010) Wave propagation in sandwich panel with auxetic core. J. Solid Mech.

[27] Zhu X, Zhang J, Zhang W, Chen J, (2019) Vibration frequencies and energies of an auxetic honeycomb sandwich plate. MAMS vol. 26, no. 23, pp. 1951-1957.