2019
DOI: 10.1016/j.compstruct.2018.11.094
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Highly accurate closed-form solutions for free vibration and eigenbuckling of rectangular nanoplates

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Cited by 18 publications
(5 citation statements)
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“…The convergence study is carried out and the results are shown in Table 1 for the square nanoplates with b = 10 nm, µ = 1 nm 2 , and k p = k p b 2 D = 20 under different BCs, including the central bending deflections, It is found that only 10 terms, at most, yield the convergence to the last digit of five significant figures for the buckling and free vibration solutions in this study, but 80 and 320 terms, at most, are needed to achieve the same accuracy for the bending solutions with uniform and concentrated loads, respectively. In Table 2, the present buckling and free vibration solutions are compared with their counterparts available in the literature by molecular dynamics simulation 2,3 , Rayleigh-Ritz method 28 , and iSOV method 31 , respectively, confirming the validity of the adopted nonlocal theory and the present method. The parameters adopted are as follows 2,3,53,54 : ρ = 2250 kg/m 3 , E = 1 TPa , ν = 0.16 , and h = 0.34 nm .…”
Section: Comprehensive Numerical Results and Discussionsupporting
confidence: 60%
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“…The convergence study is carried out and the results are shown in Table 1 for the square nanoplates with b = 10 nm, µ = 1 nm 2 , and k p = k p b 2 D = 20 under different BCs, including the central bending deflections, It is found that only 10 terms, at most, yield the convergence to the last digit of five significant figures for the buckling and free vibration solutions in this study, but 80 and 320 terms, at most, are needed to achieve the same accuracy for the bending solutions with uniform and concentrated loads, respectively. In Table 2, the present buckling and free vibration solutions are compared with their counterparts available in the literature by molecular dynamics simulation 2,3 , Rayleigh-Ritz method 28 , and iSOV method 31 , respectively, confirming the validity of the adopted nonlocal theory and the present method. The parameters adopted are as follows 2,3,53,54 : ρ = 2250 kg/m 3 , E = 1 TPa , ν = 0.16 , and h = 0.34 nm .…”
Section: Comprehensive Numerical Results and Discussionsupporting
confidence: 60%
“…The nonlocal theory-based quadratic functional for a nanoplate within the domain resting on a twoparameter elastic foundation as shown in Fig. 1a,b is written as 27,28,31 in which −h/2 ρz 2 dz , with ρ being the mass density of the nanoplate; N x and N y are the membrane forces along the x and y directions, respectively; q x, y is the transverse external load. Putting µ = 0 , the quadratic functional for the classical thin plate model is obtained.…”
Section: Governing Equation For Bending Buckling and Free Vibration Of Nanoplates In The Hamiltonian Systemmentioning
confidence: 99%
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“…Обычно исследователи не идут дальше определения первой критической нагрузки (эйлеровой), считая ее разрушающей [1][2][3][4][5][6][7], поэтому существует мало работ [8][9][10][11][12][13][14], посвященных определению начального спектра критических нагрузок и соответствующих форм потери устойчивости (форм закритического равновесия).…”
Section: Introductionunclassified
“…Khorasani et al [2] investigated the buckling problem of honeycomb sandwich panels on elastic foundations and used Navier's method to solve the governing equations. Xing et al [3][4] proposed the separated variable method for solving the buckling and vibration problems of rectangular plates.…”
Section: Introductionmentioning
confidence: 99%