1986
DOI: 10.1016/0022-460x(86)90171-9
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Natural frequencies of rectangular plates with free edges

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Cited by 34 publications
(10 citation statements)
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“…The products of eigenfunctions of vibrating beams [3][4][5][6][7] are the most commonly used two-dimensional trial functions. Other frequently used functions include degenerated beam functions [8], orthogonal characteristic beam polynomials [9][10][11][12][13][14], and spline functions [15]. The use of two-dimensional polynomials as basic functions has attracted special attention in recent years, and noteworthy works in the vibration analysis of general two-dimensional structures of arbitrary boundary conditions include those of Bhat [16], Liew and Lam [17], Liew et al [18] and Liew and Wang [19,20].…”
Section: Introductionmentioning
confidence: 99%
“…The products of eigenfunctions of vibrating beams [3][4][5][6][7] are the most commonly used two-dimensional trial functions. Other frequently used functions include degenerated beam functions [8], orthogonal characteristic beam polynomials [9][10][11][12][13][14], and spline functions [15]. The use of two-dimensional polynomials as basic functions has attracted special attention in recent years, and noteworthy works in the vibration analysis of general two-dimensional structures of arbitrary boundary conditions include those of Bhat [16], Liew and Lam [17], Liew et al [18] and Liew and Wang [19,20].…”
Section: Introductionmentioning
confidence: 99%
“…A comparison of frequency parameter Ω for homogeneous (α 1 = α 2 = β 1 = β 2 = 0) square (a/b = 1) plate of uniform (γ 1 = γ 2 = 0) thickness obtained by Rayleigh-Ritz method [7,34,37], exact and approximate results using Ritz method [33], Differential quadrature method [11,36], Optimized Kantorovich method [35] and non-uniform thickness obtained by finite element method [6], Rayleigh-Ritz method [7,9], differential quadrature method [11], optimized Kantorovich method [35] has been presented in Table 2. A close agreement of results is obtained.…”
Section: Resultsmentioning
confidence: 99%
“…, where m and n are the numbers of beam vibration nodes, then the plate mode shape function has to manifest m + n cross straight lines of zero displacement, Fig 3. Such a mesh can be noticed only in the modes 1, 8, and 17, and roughly in the modes 4,5,6,7,11,12,15,16,20,21, and 24 in Fig. 2.…”
Section: Generalmentioning
confidence: 88%