On the Missing Modes When Using the Exact Frequency Relationship between Kirchhoff and Mindlin Plates
|
|
- Melinda Foster
- 5 years ago
- Views:
Transcription
1 On the Missing Modes When Using the Eact Frequenc Relationship between Kirchhoff and Mindlin Plates C.W. Lim 1,*, Z.R. Li 1, Y. Xiang, G.W. Wei 3 and C.M. Wang 4 1 Department of Building and Construction, Cit Universit of Hong Kong, Tat Chee Avenue, Kowloon, Hong Kong School of Engineering and Industrial Design & Centre for Construction Technolog and Research, Universit of Western Sdne, Penrith South DC, NSW 1797, Australia 3 Department of Mathematics and Department of Electrical and Computer Engineering, Michigan State Universit, East Lansing, MI 4884, U.S.A. 4 Department of Civil Engineering, National Universit of Singapore, Kent Ridge, Singapore Abstract An eact frequenc relationship eists between Kirchhoff and Mindlin plates of polgonal planform and simpl supported edges. In this paper, we show that the use of this relationship leads to missing vibration modes due to the lack of consideration for the transverse shear modes and coupled bending-shear modes in the relationship. The missing modes appear at relativel high order modes and the were originall discovered b using discrete singular convolution (DSC) method that is capable of accuratel predicting thousands of vibration modes without suffering from numerical instabilit as other methods do. An efficient state-space technique is used to confirm our findings. Using the state-space technique, eact vibration frequencies for transverse shear vibration modes of thick plates can be obtained. Numerical eamples are presented to support our claims. These eact shear frequencies complement the bending frequencies predicted b using the Kirchhoff-Mindlin relationship. It is interesting to note that there are some coupled bending-shear modes that can picked up b the DSC method which provides a complete spectrum of frequencies, even for ver high frequencies. Kewords: discrete singular convolution, high frequenc, Kirchhoff-Mindlin relationship, transverse shear mode, state-space, thick plate, vibration. * Corresponding author: C.W. Lim, Department of Building and Construction, Cit Universit of Hong Kong, Tat Chee Avenue, Kowloon, Hong Kong, P.R. China. bccwlim@citu.edu.hk
2 1. Introduction The Kirchhoff (or classical thin) plate theor [1,] is the simplest and most commonl used plate theor for bending, vibration and buckling analses of plates. This theor, however, neglects the effect of transverse shear deformation b the simplified assumption that the normals to the undeformed midplane remain normal after deformation. This theor leads to an overprediction of buckling loads and natural vibration frequencies and an underprediction of deflections when applied to thick plates because of the significant effect of transverse shear deformation in such plates. In 1951, Mindlin [3,4] proposed the first order shear deformation plate theor that relaes the aforementioned normalit assumption. B allowing the straight normals to rotate with respect to the mid-plane of the deformed plate, a constant shear strain is admitted through the plate thickness. This relaation produces two additional degrees of freedom, i.e. the angles of rotation in the two perpendicular directions, in the plate modeling. Owing to the additional degrees of freedom, various analtical solution methodologies applicable to the Kirchhoff plate analsis become invalid and man eact analses available in Kirchhoff plate models cannot be etended to the Mindlin (or thick) plate analsis. In view of the aforementioned problems, Wang and his coauthors [5-9] initiated studies to relate the solutions of Kirchhoff (or thin) plate theor and Mindlin (or thick) plate theor. The derived eact relationships between the two models in bending [5], buckling [6] and vibration [7-9]. Such Kirchhoff-Mindlin relationships ehibit a one-to-one mapping of the eact solutions in both plate models. Consequentl man known eact solutions of thin plates can be easil converted to eact thick plate solutions and these eact relationships can be easil handled b practicing engineers who need not have too much knowledge in the thick plate theor. Nevertheless, there are some inherent pitfalls when using these eact relationships, which is the subject of the present paper. Here, our concern is the missing shear modes in thick plate vibration. As the relationships assume a one-to-one mapping, man phsical modes that eist when the thickness of plate becomes relativel high ma not be captured. The missing modes are due to transverse shear deformation and coupled bending-shear
3 deformation in thick plate dnamics. If care is not taken while appling the Kirchhoff-Mindlin relationships, important phsical features of the thick plate ma not be realized and thus the results ma be insufficientl interpreted. To analze the missing shear modes, an efficient state-space technique is presented in this paper to derive a sstem of homogenous differential equation for the vibration of a thick plate considering onl the transverse shear deformable modes. This method has been shown to be ver effective in furnishing eact solutions for bending and vibration of plates and clindrical shells [10-1]. It is etended here for the analsis of transverse shear vibration modes of thick plates. Eact shear frequenc solutions are obtained for plates with two opposite sides simpl supported. The eact shear modes complement the bending frequencies predicted from the Kirchhof-Mindlin relationship. However, there are some modes due to the coupling between the bending and the shear dnamics that can not be predicted b the relationship. The can be recovered from the discrete singular convolution (DSC) methods which deliver a complete frequenc spectrum for the vibration analsis of thick Mindlin plates. In addition, the influence of plate boundar conditions on the shear vibration frequencies is eamined. The DSC [13-18] method is another potential numerical approach for plate analses. It is regarded as a novel approach for numerical analsis of singular integrations. The mathematical underpinning of the DSC algorithm is the theor of distributions and wavelet analsis. Man DSC kernels, such as the (regularized) Shannon delta sequence kernel, the (regularized) Dirichlet delta sequence kernel, the (regularized) Lagrange delta sequence kernel and the (regularized) de la Vallée Poussin delta sequence kernel, have been constructed [16]. B appropriatel selecting kernel parameters, the DSC approach ehibits controllable accurac for integration and ecellent fleibilit in handling comple geometries and boundar conditions. In this paper, a complete spectrum of vibration frequencies is resolved using the DSC collocation (DSC-CO) method and the DSC-Ritz method where the latter is an etension of the Ritz procedure using DSC kernels. 3
4 . Modelling and Formulation.1. Problem Definition Consider an isotropic, elastic, rectangular plate of uniform thickness h, length a, width b, Young s modulus E, shear modulus G, Poisson s ratio ν and mass densit ρ, as shown in Fig. 1. The plate is simpl supported on two opposite sides and the other two sides ma assume free, simpl supported or clamped. Here, we intend to determine the vibration frequencies of the plate using three different approaches: (i) the Kirchhoff-Mindlin relationship for bending vibration modes; (ii) the DSC-CO method and the DSC-Ritz method; and (iii) the state-space formulation for shear vibration modes... Frequenc Relationship of Kirchhoff and Mindlin Plates The eact frequencies for the vibration of a simpl supported, rectangular Kirchhoff (or thin) plate are given b [] ω i mπ nπ ( ) ( ) = + / ρh / D a b where i = 1,,, corresponds to the mode sequence number and m, n are the number of half number of half waves. The corresponding frequenc for a Mindlin plate can be deduced via a formal relationship given b [7,8] 6κ G 1 ρh 1 ρh ρh ωi = 1+ ωih ϒ 1+ ωih ϒ 1 D 1 D ω ρh 3κ G ϒ = 1 + κ ( 1 µ ) i (1) () where ω i correspond to the frequenc a Mindlin plate of the same dimensions and material properties, and κ is the shear correction factor.. From Eq. (), accurate frequencies for a simpl supported Mindlin plate can be derived from the Kirchhoff plate solutions given b Eq. (1). These are the fleural vibration modes where a one-to-one mapping between the Kirchhoff plate and the Mindlin plate is possible..3. DSC-Ritz and DSC-CO Formulation Let T denotes a singular kernel and η ( ) be an element of the space of test functions. A singular convolution is defined as 4
5 + Ft () = ( T* η)() t = Tt ( ) η( d ) (3) where t indicates the time variable and a dumm variable. Depending on the form of the kernel T, the singular convolution is the ke issue for a wide range of problems in science and engineering, e.g., Hilbert transform, Abel transform, and Radon transform. However singular kernels cannot be directl applied in computers because the are tempered distributions and do not have a value anwhere. Hence, the singular convolution in Eq. (3) is of little direct numerical merit. In order to avoid the difficult of using singular epressions directl in computer, we need to construct sequences of approimations ( T α ) to the distribution T lim Tα ( ) T( ), (4) α α 0 where α 0 is a generalized limit. Obviousl, for the singular kernels of the delta tpe, T ( ) = δ( ), each element in the sequence, T ( ), is a delta sequence kernel. With a sufficientl smooth approimation, it is useful to consider a discrete singular convolution (DSC) F () t = T ( t )( f ) α k α where Fα () t is the approimation of Ft () and { k } is an appropriate set of discrete points on which the DSC in Eq. (5) is well defined. Note that, the original test function η ( ) is replaced b f. ( ) k α k (5) As the Fourier transform of the delta distribution is unit in the Fourier domain, the distribution can be regarded as a universal reproducing kernel [13] f ( ) = δ ( ) f ( ) d (6) As a consequence, delta sequence kernels are approimate reproducing kernels or bandlimited reproducing kernels that provide a good approimation to the universal reproducing kernel in certain frequenc bands. There are man delta sequence kernels arising in the theor of partial differential equations, Fourier transforms, signal processing and wavelet analsis, with completel 5
6 different mathematical properties. For the purpose of numerical computations, the delta sequence kernels of both (i) positive tpe and (ii) Dirichlet tpe are of particular importance and the have ver distinct mathematical and numerical properties. For simplicit, we focus on two tpical kernels of the Dirichlet tpe, Shannon s delta sequence kernel sin( α) δα( ) = (7) π and a simplified de la Vallée Poussin delta kernel 1 cos( α) cos( α) δα() = πα (8) to realize the proposed DSC method. According to the theor of distributions, the smoothness, regularit and localization of a tempered distribution can be improved b a function of the Schwartz class. It is suggested in [19] that a delta regularizer Rσ () is used in regularizing a delta kernel. A good eample is the Gaussian R ( ) = e σ σ Therefore, Shannon s delta sequence kernel in Eq. (7) and de la Vallée Poussin delta kernel in Eq. (8) can be modified in their regularized form as (9) and δ σα, ( ) sin( α) e π = σ (10) δ ( ) 1 cos( α) cos( α) πα = e σ (11) σα, These regularized kernels converge etremel fast when used for approimating functions and their derivatives. For practical computational purposes, the can be truncated for a finite domain. For different implementations of the DSC algorithm, the two popular methods are the 6
7 Ritz method and the collocation formulation. The DSC-collocation is a local method, in which the derivative of a function at a particular point in the coordinate domain is computed b as a few neighborhood grid points. While the Ritz method is classicall a global method, it requires the full set of grid points in a computational domain to compute a derivative. However, the DSC-Ritz can be formulated as a local method because the DSC kernels have time-frequenc localization. The Ritz approach to the Mindlin plate vibration problem is based on the energ principle. B assuming a set of admissible trial functions with independent amplitude coefficients, a closer upper bound for the frequenc could be achieved b minimizing the energ functional with respect to the coefficients. In the DSC-Ritz method, a new set of trial functions is emploed, which is able to approimate the deflection of the whole domain and at the same time satisfies the prescribed boundar conditions. These trial functions are formed from the product of sets of two-dimensional localized DSC kernels and basic functions which associate the piecewise boundar geometric epressions. The new shape α k functions ϕ ( α = w, θ, θ ) can be epressed as α α k k l ϕ (, ξ η) = f (, ξ η) ϕ (1) where b ϕ b α is the basic function. The two-dimensional DSC kernel M N N fk = k= 1 i= 1 j= 1 M fk (, ξη) are given k = 1 (, ξη) δσij(, ξη) (13) where N is the number of grid points adopted in both ξ- direction and η- direction, and M = N, k = ( i -1) N + j (14) Note that δ σij in Eq. (13) is a DSC delta kernel and the two-dimensional forms for the aforementioned two DSC kernels in Eqs. (10-11) can be constructed b tensor products as δ σij (, ξ η) = for Shannon s kernel, and sin[( π/ )( ξ ξi)]sin[( π/ )( η ηj)] e ( π / )( ξ ξ )( η η ) i j i i [( ξ ξ ) / σ ] [( η η ) / σ ] e (15) 7
8 δ σij (, ξ η) = cos[( π/ )( ξ ξi)] cos[( π/ )( ξ ξi)] e ( π/ )( ξ ξi ) cos[( π/ )( η ηj)] cos[( π/ )( η ηj)] e ( π/ )( η ηj ) i [( ξ ξ ) / σ ] j [( η η ) / σ ] for de la Vallée Poussin kernel. In all the above kernels, ξ i and η j are grid point along the ξ- ais and η- ais, respectivel. The parameters σ and are chosen as (16) σ = r ; 3 =, where is the grid spacing, and r is an adjustable parameter determining the radius of influence. Details on how to accommodate the geometric boundar conditions are given b Lim et al. [18, 0, 1]. For the DSC-CO method, the solution of the Mindlin plate vibration problem is obtained b directl solving the discretized partial differential equations. In the DSC-CO, the approimate solution is sought from a finite set of N DSC kernel functions. Numericall to solve the plate vibration governing equation, it is necessar to give a matri approimation to the differential operator so that the action of the operator can be realized. The DSC approimation to the n th order derivative of a function ϕ ( α = w, θ, θ ) can be rewritten as n kl B n α k+ M ϕ n α n q= q = c k kl, Bϕ q (17) l= k M where c, are a set of DSC weights and can be calculated through the DSC kernel, and q is the direction of differentiation ( q = ξη, ), and n ( = 0,1,, ) is the order of differentiation. The regularized Shannon kernel is used in the present work. B substituting Eq. (17) into the governing differential equations, a sstem of linear algebraic equations for the governing equations can be obtained. Before calculating the eigenvalues, appropriate boundar conditions are to be implemented. The reader is referred to Refs. [15] and [16] for an elaboration about the DSC-CO method and its applications. α 8
9 .4. Eact Solution for Shear Vibration of Thick Plates Considering onl the magnitude of vibration where the time dependent function sinω t has been simplified, the governing differential equations for a thick plate based on the Mindlin plate theor can be epressed as [4] w w κ Gh + θ + + θ + ρhω w = 0 (18) 3 (1 ) D w h D θ θ ν θ θ ρ ν κ Gh + θ + ω θ = 0 1 (19) 3 (1 ) D w h D θ θ ν θ θ ρ ν κ Gh + θ + ω θ = 0 1 where θ (, ), (, ) (0) θ are rotations in the -ais and -ais, w (, ) is the transverse displacement, D Eh 3 1( 1 ν ) frequenc, and = is the fleural rigidit, ω is the angular κ is the shear correction factor. If the plate vibrates in a shear mode, i.e. w(, ) = 0, the governing differential equations reduce to 3 (1 ) D h D θ θ ν θ θ ρ ν κ Ghθ + ω θ = 0 1 (1) 3 (1 ) D h D θ θ ν θ θ ρ ν κ Ghθ + ω θ = 0 1 () For a simpl supported rectangular plate of side length a and width b, the rotations in Eqs. (1) and () can be epressed as nπ mπ θ (, ) = Acos sin (3) a b nπ mπ θ (, ) = Bsin cos (4) a b where n and m are the number of halfwaves of the vibration mode along the and directions, and A and B are unknown coefficients to be determined, respectivel. B 9
10 substituting Eqs. (3) and (4) into Eqs. (1) and (), the non-trivial frequenc ω can be obtained eplicitl and epressed in terms of the non-dimensional frequenc parameter λ ( = ( ωb / π ) ρh / D) as follows b m π h n π h λ = ν κ + + π h b a 6(1 ) 1 where a/ b is the aspect ratio and h/ b is the thickness ratio of the plate, respectivel. (5) For a plate with simpl supported edges opposite to each other, the state-space technique must be adopted to obtain the eact solutions. Assuming that the two simpl supported edges are parallel to the -ais, the rotations in Eqs. (1) and () can be epressed as []: mπ θ (, ) = φ ( ) sin (6) b mπ θ (, ) = φ ( ) cos (7) b where φ () and φ ( ) are unknown functions to be determined. Equations. (6) and (7) satisf the simpl supported boundar conditions on edges at = 0 and = b. B substituting Eqs. (6) and (7) into Eqs. (1) and (), the following differential equation sstem can be derived ( ψ )' = Hψ (8) where ψ = [ φ ' ' T ( φ ) φ ( φ ) ], the prime represents the derivative with respect to and H is a 4 4 matri with the following non-zero elements: H = H 1 (9) 1 34 = H 1 D(1 ν )( mπ / b) / + κ Gh ρhω /1 = (30) D ( mπ / b)(1 +ν ) H 4 = (31) ( mπ / b)(1 + ν ) H 4 = 1 ν (3) 10
11 3 D( mπ / b) + κ Gh ρh ω /1 H 43 = (33) [ D(1 ν ) / ] A general solution of Eq. (8) can be obtained as H ψ = e c (34) where c is a 4 1 constant vector that can be determined b the boundar conditions of the two edges parallel to the -ais and i H e is the general matri solution of Eq. (8) []. The two edges parallel to the -ais ma have the following prescribed boundar conditions when the shear vibration of the plate is considered M 0, M = 0, if the edge is free (35,36) = = M 0, θ = 0 if the edge is simpl supported (37,38) θ 0, θ = 0 if the edge is clamped (39,40) = where M and M are bending moment and twisting moment in the plate, respectivel, and are defined b M θ = D θ + ν (41) M 1 ν θ = D θ + (4) In view of Eq. (34), a homogeneous sstem of equations can be derived b implementing the boundar conditions of the plate along the two edges parallel to the -ais [Eqs. (35)-(40)] and is given b Kc = 0 (43) where K is a 4 4 matri. The vibration frequenc ω ma be determined when the determinant of K in Eq. (6) is equal to zero. 11
12 3. Numerical Eamples In this section, a few numerical eperiments are designed to illustrate the missing modes when using the Kirchhoff-Mindlin relationship for determining shear related vibration modes. 3.1 Simpl supported (SSSS) thick plate Table 1 shows the dimensionless frequencies obtained using the Kirchhoff-Mindlin relationship, eact shear mode solutions from Eq. (5), DSC-Ritz method and DSC-CO method for a plate with a thickness ratio h/ a = 0.1. Prior to mode-113, the Kirchhoff-Mindlin relationship provides eact mapping with respect to the solutions of DSC-Ritz and DSC-CO indicating that there eist no transverse shear modes in this range. At mode 113 and beond, the mismatch begins to appear. As shown in Table 1, modes-113 to 115 are pure transverse shear modes corresponding to (0,1), (1,0) and (1,1) for the half-wave numbers denoted b ( mn, ). The number of missing modes increases for higher frequencies because the shear effect becomes more and more significant when the wavelength becomes shorter. Although the mismatch of frequencies onl appears from mode-113, it is epected that mismatches occur at much lower modes if the plate is thicker. To prove this prediction, two more eamples for the SSSS plate are presented in Tables and 3, in which the thickness ratios are ha= 0. and 0.5 respectivel. Indeed, the transverse shear modes start to appear as low as at mode-7 and mode-18, respectivel. It is epected that the transverse shear modes begin to dominate the lower order modes when thickness of the plate is further increased. It is interesting to note that there eists another class of coupled bending-shear vibration modes involving coupled terms of w θ or w θ besides the pure bending and pure transverse shear modes as indicated in Table 1. These modes cannot be predicted b the Kirchhoff-Mindlin relationship because the θ or θ effects are not considered nor the be predicted b the eact shear mode solutions from Eq. (5) because the fleural effect is not considered. It is also 1
13 observed that a complete spectrum of accurate frequenc solutions can be furnished b both the DSC-Ritz and DSC-CO methods. The latter method ehibits better accurac when compared to the eact solutions of the Kirchhoff-Mindlin relationship and the eact shear mode solutions. Therefore, DSC-Ritz and DSC-CO are potential methods for analzing high frequencies in regions where no eact solution eists or other numerical methods, such as the finite element method, encounter failure. For more information on the high frequenc analsis, please refer to Lim et al. [18]. 3. Other thick plates with two opposite sides simple supported (SFSF and SCSC) To further illustrate the potential of the DSC-Ritz algorithm, two more eamples for thick plates are presented. These are plates with two opposite sides simpl supported, while the other two sides ma be free (named SFSF plate), or clamped (named SCSC plate). These results are presented in Tables 4 and 5, respectivel. Here, the eact Kirchhoff-Mindlin frequenc relationships are not available. As there is no eplicit analtical solution such as that in Eq. (5) available, the state space technique presented in Sec..4 needs to be emploed to obtain numerical shear mode solutions b solving Eq. (43). Matching of the shears modes from the state space technique with the complete frequenc spectrum as presented in Tables 4 and 5 ma create confusion. However, bearing in mind that the Ritz method alwas overestimates the vibration frequencies, the matching has been done such that the DSC-Ritz solutions are alwas a little higher that the state space solutions. The pure transverse shear modes start to appear at mode-38 and mode-30, respectivel, for the SFSF and SCSC plates. These eamples, again, clearl demonstrate that pure shear vibration modes do eist and an eact relationships linking the Kirchhoff and Mindlin plates, if available in the future, must be implemented in care. To help understand the phsical nature of pure shear vibration modes, two eamples are presented in Figs. and 3 for a square simpl supported plate with ab= 1, hb= 0.1, n = 3, m = (for Fig. ) and m = 3 (for Fig. 3), respectivel. As observed, these vibration modes onl involve deformation in planes parallel to the mid-plane of the plate caused b shear deformation or rotation of the normals originall perpendicular to the 13
14 mid-plane. It is also obvious that such modes vibrate at a lower frequenc if the plate is thicker. 4. Conclusions This paper addresses the missing vibration modes of thick Mindlin plates when using a Kirchhoff-Mindlin frequenc relationship. The relationship, valid for simpl supported and polgonal plates, gives a one-to-one mapping of vibration frequencies between a Kirchhoff plate and a Mindlin plate. It has been served as a useful and convenient tool for analzing complicated thick plates based on the simple thin plate theor. However, the limitation of such a relationship has not been detected previousl. As the Kirchhoff plate accounts onl for the bending effect, the transverse shear dnamics is neglected and it plas an important role in the frequenc spectrum of Mindlin plates. The pure shear modes are predicted b a state-space technique and are found to complement the bending modes predicted b the relationship. The state-space technique is capable of providing eact frequenc parameters for the Mindlin plates. A complete and accurate vibration spectrum of the thick Mindlin plates, including the modes due to bending, shear, and their coupling, are obtained b using discrete singular convolution (DSC) methods, with which the missing modes were original discovered. Numerical eamples are designed to support the present claim. Further findings include the fact that the pure transverse shear modes and mode coupling between shear and bending enter into the lower order mode ranges as the thickness of the Mindlin plate increases. Acknowledgement This research is supported in part b a Young/Junior Scholars (YSS) Funding of the Cit Universit of Hong Kong. The authors wish to thank Dr Yibao Zhao for providing the DSC-CO results. 14
15 References 1. Timoshenko SP, Woinowsk-Krieger S. Theor of plates and shells, nd ed., McGraw-Hill: New York, Leissa AW. Vibration of plates. NASA SP-160, Scientific and Technical Information Office, NASA: Washington DC, Reissner E. The effct of transverse shears deformation on the bending of elastic plate. Journal of Applied Mechanics 1945; 1: Mindlin RD. Influence of rotar inertia and shear in fleural motion of isotropic, elastic plates. Journal of Applied Mechanics 1951; 18: Wang CM, Redd JN and Lee KH. Shear Deformable Beams and Plates: Relationships with Classical Solutions, Elsevier: Singapore, Redd JN, Wang CM. Relationship between classical and shear deformation theories on aismmetric circular plates. AIAA Journal 1997; 35: Wang CM. Natural frequencies formula for simpl supported Mindlin plates. Journal of Vibration and Acoustics 1994; 116: Liew KM, Wang CM, Xiang Y, Kitipornchai S. Vibration of Mindlin Plates: Programming the p-version Ritz Method. Elsevier: Oford, Wang CM. Vibration frequencies of simpl supported polgonal sandwich plates via Kirchhoff solutions. Journal of Vibration and Vibration 1996; 190: Xiang Y, Wang CM. Eact buckling and vibration solutions for stepped rectangular plates. Journal of Sound and Vibration 00; 50: Xiang Y, Wang CM, Kitipornchai S. Eact buckling solutions for rectangular plates under intermediate and end uniaial loads. Journal of Engineering Mechanics, ASCE, 003, 19: Xiang Y, Ma YF, Kitipornchai S, Lim CW, Lau CWH. Eact solutions for vibration of clindrical shells with intermediate ring supports. International Journal of Mechanical Sciences 00, 44: Wei GW. Discrete singular convolution for the solution of the Fokker-Planck equations. Journal of Chemical Phsics 1999; 110: Wei GW. Wavelets generated b the discrete singular convolution kernels. Journal of Phsics A 000; 33: Wei GW. Vibration analsis b discrete singular convolution. Journal of Sound and Vibration 001; 44: Wei GW, Zhao YB, Xiang Y. Discrete singular convolution and its application to the analsis of plates with internal supports. I Theor and algorithm. International Journal for Numerical Methods in Engineering 00;55: Xiang Y, Zhao YB, Wei GW. Discrete singular convolution and its application to the analsis of plates with internal supports. II Comple supports. International Journal for Numerical Methods in Engineering 00;55: Lim CW, Li ZR and Wei GW, DSC-Ritz method for high-mode frequenc analsis of thick shallow shells, I. J. Num. Meth. Eng., in press, Wei GW, Zhang DS, Kouri DJ, Hoffman DK. Lagrange distributed approimating functionals. Phsical Review Letters 1997; 79: Liew KM, Lim CW. A Ritz vibration analsis of doubl-curved rectangular shallow shells using a refined first-order theor. Computer Methods in Applied Mechanics and Engineering 1995; 17:
16 1. Liew KM, Lim CW. Vibration studies on moderatel thick doubl-curved elliptic shallow shells. Acta Mechanica 1996; 116: Xiang, Y, Wei, GW. Eact solutions for buckling and vibration of stepped rectangular Mindlin plates. International Journal of Solids and Structures 004; 41:
17 Table 1. Comparison of frequenc parameter λ ωa ρh/ D / π = for an SSSS thick square Mindlin plate with ν = 0.3 and h/ a = 0.1. Values in parenthesis indicate the mode sequence number corresponding to Kirchhoff-Mindlin relationship [8]. Kirchhoff-Mindlin Eact solutions for DSC-Ritz Method Mode DSC-CO Relationship pure transverse number de la Vallée Shannon Method (mode number) Shear modes (m,n) Poussin (0,1) (1,0) (1,1) (113) (114) (0,) (,0) (1,) (,1) (115) (116) (117) (,) (0,3) (3,0) (118) (119) (1,3) (3,1) (10) (11) (1) (13) (14) (15) (,3) (3,) (0,4) (4,0) (16) (17) (1,4) (4,1) (3,3) (18) (19) (130) (131) (,4) (4,) (13) (133) (134) (135) (0,5) (5,0) (3,4) (4,3) (1,5)
18 (5,1) (136) (137) (,5) (5,) (138) (139) (140) (141) (4,4) (14) (143) (144) (3,5) (5,3) (145) (146) (0,6) (6,0) (1,6) (6,1) (147) (148) (149) (150) (,6) (6,) (151) (15) (5,4) (4,5) (153) (154) (01) (8,9) (0,14) (341) (386) (11,15) (6,19) (11,18) Coupled bending-transverse shear ( w θ or w θ ) vibration modes 18
19 Table. Comparison of frequenc parameter λ ωa ρh/ D / π = for an SSSS thick square Mindlin plate with ν = 0.3 and h/ a = 0.. Values in parenthesis indicate the mode sequence number corresponding to Kirchhoff-Mindlin relationship [8]. Mode number Kirchhoff-Mindlin Relationship (mode number) Eact solutions for pure transverse shear modes (m,n) DSC-Ritz Method Shannon De la Vallée Poussin (1) () (3) (4) (5) (6) (7) (8) (9) (10) (11) (1) (13) (14) (15) (16) (17) (18) (19) (0) (1) () (3) (4) (5) (6) (0,1) (1,0) (7) (8) (1,1) (0,) (,0) (9) (30) (1,) (,1) (,) (31) (3) (33) (0,3) (3,0) (1,3) (3,1) (34) (35) (36) (37) (,3) (3,)
20 (38) (39) (0,4) (4,0) (1,4) (4,1) (40) (41) (3,3) (,4) (4,) (4) (43) (44) (45) (46) (47) (0,5) (3,4) (4,3) (5,0) (1,5) (5,1) (48) (49) (50) (51) (5) (,5) (5,) (4,4) (53) (54) (3,5) (5,3) (55) (56) (0,6) (6,0) (57) (58) (59) (60) Coupled bending-transverse shear ( w θ or w θ ) vibration modes 0
21 Table 3. Comparison of frequenc parameter λ ωa ρh/ D / π = for an SSSS thick square Mindlin plate with ν = 0.3 and h/ a = 0.5. Values in parenthesis indicate the mode sequence number corresponding to Kirchhoff-Mindlin relationship [8]. Mode number Kirchhoff-Mindlin Relationship (mode number) Eact solutions for pure transverse shear modes (m,n) DSC-Ritz Method Shannon de la Vallée Poussin (1) () (3) (4) (5) (6) (7) (8) (9) (10) (11) (1) (13) (14) (15) (16) (17) (0,1) (1,0) (1,1) (18) (19) (0,) (,0) (1,) (,1) (0) (1) () (,) (0,3) (3,0) (3) (4) (1,3) (3,1) (5) (6) (7) (8) (,3) (3,) (9) (30) (0,4) (4,0) (1,4) (4,1) (3,3)
22 (31) (3) (33) (,4) (4,) (34) (35) (36) (37) (0,5) (3,4) (4,3) (5,0) (1,5) (5,1) (38) (39) (40) (41) (,5) (5,) (4,4) (4) (43) (44) (45) (3,5) (5,3) (46) (47) (0,6) (6,0) (1,6) (6,1) (48) (49) (50) (51) (5) (6,) (,6) (4,5) (5,4) Coupled bending-transverse shear ( w θ or w θ ) vibration modes
23 Table 4. Comparison of frequenc parameter λ ωa ρh/ D / π = for an SFSF thick square Mindlin plate with ν = 0.3 and h/ a = 0.. Mode number Pure transverse shear modes via state space method (m,n) DSC-Ritz Method Shannon de la Vallée Poussin (1,1) (1,) (,1) (1,3) (1,4) (,) (1,5) (3,1) (3,) (,3)
24 (1,6) (,4) (3,3) (4,1) (4,) (,5) (,6) (1,7) (1,8) (3,4) (4,3) (5,1) (,7) (5,) (,8) (3,5) (4,4) (3,6) (1,9) (5,3) (1,10) (6,1) (6,) (3,7)
25 Table 5. Comparison of frequenc parameter λ ωa ρh/ D / π = for an SCSC thick square Mindlin plate with ν = 0.3 and h/ a = 0.. Mode number Pure transverse shear modes via state space method (m,n) DSC-Ritz Method Shannon de la Vallée Poussin (1,1) (1,) (,1) (1,3) (,) (1,4) (3,1) (,3) (,4) (3,) (1,5) (1,6)
26 (4,1) (3,3) (,5) (4,) (,6) (3,4) (1,7) (5,1) (4,3) (1,8) (5,) (3,5) (,7) (3,6) (,8) (4,4) (5,3) (6,1) (1,9)
27 z b a h Fig. 1. Geometr of a thick plate. 7
28 Fig.. Pure shear vibration mode for a square simpl supported plate with ab= 1, hb= 0.1, n = 3, m = and λ = Fig. 3. Pure shear vibration mode for a square simpl supported plate with ab= 1, hb= 0.1, n = 3, m = 3 and λ =
Vibration Analysis of Isotropic and Orthotropic Plates with Mixed Boundary Conditions
Tamkang Journal of Science and Engineering, Vol. 6, No. 4, pp. 7-6 (003) 7 Vibration Analsis of Isotropic and Orthotropic Plates with Mied Boundar Conditions Ming-Hung Hsu epartment of Electronic Engineering
More informationVibration of Plate on Foundation with Four Edges Free by Finite Cosine Integral Transform Method
854 Vibration of Plate on Foundation with Four Edges Free b Finite Cosine Integral Transform Method Abstract The analtical solutions for the natural frequencies and mode shapes of the rectangular plate
More informationNote on Mathematical Development of Plate Theories
Advanced Studies in Theoretical Phsics Vol. 9, 015, no. 1, 47-55 HIKARI Ltd,.m-hikari.com http://d.doi.org/10.1988/astp.015.411150 Note on athematical Development of Plate Theories Patiphan Chantaraichit
More informationFree Vibration Analysis of Rectangular Plates Using a New Triangular Shear Flexible Finite Element
International Journal of Emerging Engineering Research and echnolog Volume Issue August PP - ISSN - (Print) & ISSN - (Online) Free Vibration Analsis of Rectangular Plates Using a New riangular Shear Fleible
More informationVibrational Power Flow Considerations Arising From Multi-Dimensional Isolators. Abstract
Vibrational Power Flow Considerations Arising From Multi-Dimensional Isolators Rajendra Singh and Seungbo Kim The Ohio State Universit Columbus, OH 4321-117, USA Abstract Much of the vibration isolation
More informationChapter 6 2D Elements Plate Elements
Institute of Structural Engineering Page 1 Chapter 6 2D Elements Plate Elements Method of Finite Elements I Institute of Structural Engineering Page 2 Continuum Elements Plane Stress Plane Strain Toda
More informationLATERAL BUCKLING ANALYSIS OF ANGLED FRAMES WITH THIN-WALLED I-BEAMS
Journal of arine Science and J.-D. Technolog, Yau: ateral Vol. Buckling 17, No. Analsis 1, pp. 9-33 of Angled (009) Frames with Thin-Walled I-Beams 9 ATERA BUCKING ANAYSIS OF ANGED FRAES WITH THIN-WAED
More informationShear and torsion correction factors of Timoshenko beam model for generic cross sections
Shear and torsion correction factors of Timoshenko beam model for generic cross sections Jouni Freund*, Alp Karakoç Online Publication Date: 15 Oct 2015 URL: http://www.jresm.org/archive/resm2015.19me0827.html
More informationtorsion equations for lateral BucKling ns trahair research report r964 July 2016 issn school of civil engineering
TORSION EQUATIONS FOR ATERA BUCKING NS TRAHAIR RESEARCH REPORT R96 Jul 6 ISSN 8-78 SCHOO OF CIVI ENGINEERING SCHOO OF CIVI ENGINEERING TORSION EQUATIONS FOR ATERA BUCKING RESEARCH REPORT R96 NS TRAHAIR
More informationStrain Transformation and Rosette Gage Theory
Strain Transformation and Rosette Gage Theor It is often desired to measure the full state of strain on the surface of a part, that is to measure not onl the two etensional strains, and, but also the shear
More informationBending of Shear Deformable Plates Resting on Winkler Foundations According to Trigonometric Plate Theory
J. Appl. Comput. ech., 4(3) (018) 187-01 DOI: 10.055/JAC.017.3057.1148 ISSN: 383-4536 jacm.scu.ac.ir Bending of Shear Deformable Plates Resting on Winkler Foundations According to Trigonometric Plate Theor
More informationSurvey of Wave Types and Characteristics
Seminar: Vibrations and Structure-Borne Sound in Civil Engineering Theor and Applications Surve of Wave Tpes and Characteristics Xiuu Gao April 1 st, 2006 Abstract Mechanical waves are waves which propagate
More informationClosed form solutions for free vibrations of rectangular Mindlin plates
Acta Mech Sin (2009) 25:689 698 DOI 10.1007/s10409-009-0253-7 RESEARCH PAPER Closed form solutions for free vibrations of rectangular Mindlin plates Yufeng Xing Bo Liu Received: 26 June 2008 / Revised:
More informationAircraft Structures Structural & Loading Discontinuities
Universit of Liège Aerospace & Mechanical Engineering Aircraft Structures Structural & Loading Discontinuities Ludovic Noels Computational & Multiscale Mechanics of Materials CM3 http://www.ltas-cm3.ulg.ac.be/
More informationBending of Simply Supported Isotropic and Composite Laminate Plates
Bending of Simply Supported Isotropic and Composite Laminate Plates Ernesto Gutierrez-Miravete 1 Isotropic Plates Consider simply a supported rectangular plate of isotropic material (length a, width b,
More informationInternational Journal of Technical Research and Applications Tushar Choudhary, Ashwini Kumar Abstract
International Journal of Technical Research and Applications e-issn: 30-8163 www.ijtra.com Volume 3 Issue 1 (Jan-Feb 015) PP. 135-140 VIBRATION ANALYSIS OF STIFF PLATE WITH CUTOUT Tushar Choudhar Ashwini
More informationCH.7. PLANE LINEAR ELASTICITY. Multimedia Course on Continuum Mechanics
CH.7. PLANE LINEAR ELASTICITY Multimedia Course on Continuum Mechanics Overview Plane Linear Elasticit Theor Plane Stress Simplifing Hpothesis Strain Field Constitutive Equation Displacement Field The
More informationMathematical aspects of mechanical systems eigentones
Seminar: Vibrations and Structure-Borne Sound in Civil Engineering Theor and Applications Mathematical aspects of mechanical sstems eigentones Andre Kuzmin April st 6 Abstract Computational methods of
More informationPLATE AND PANEL STRUCTURES OF ISOTROPIC, COMPOSITE AND PIEZOELECTRIC MATERIALS, INCLUDING SANDWICH CONSTRUCTION
PLATE AND PANEL STRUCTURES OF ISOTROPIC, COMPOSITE AND PIEZOELECTRIC MATERIALS, INCLUDING SANDWICH CONSTRUCTION SOLID MECHANICS AND ITS APPLICATIONS Volume 10 Series Editor: G.M.L. GLADWELL Department
More informationStress and Strain ( , 3.14) MAE 316 Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering
(3.8-3.1, 3.14) MAE 316 Strength of Mechanical Components NC State Universit Department of Mechanical & Aerospace Engineering 1 Introduction MAE 316 is a continuation of MAE 314 (solid mechanics) Review
More informationEstimation Of Linearised Fluid Film Coefficients In A Rotor Bearing System Subjected To Random Excitation
Estimation Of Linearised Fluid Film Coefficients In A Rotor Bearing Sstem Subjected To Random Ecitation Arshad. Khan and Ahmad A. Khan Department of Mechanical Engineering Z.. College of Engineering &
More informationApplications of Gauss-Radau and Gauss-Lobatto Numerical Integrations Over a Four Node Quadrilateral Finite Element
Avaiable online at www.banglaol.info angladesh J. Sci. Ind. Res. (), 77-86, 008 ANGLADESH JOURNAL OF SCIENTIFIC AND INDUSTRIAL RESEARCH CSIR E-mail: bsir07gmail.com Abstract Applications of Gauss-Radau
More informationTransient vibration analysis of a completely free plate using modes obtained by Gorman s Superposition Method
Transient vibration analysis of a completely free plate using modes obtained by Gorman s Superposition Method Y Mochida *, S Ilanko Department of Engineering, The University of Waikato, Te Whare Wananga
More informationClosed form expressions for the gravitational inner multipole moments of homogeneous elementary solids
Closed form epressions for the gravitational inner multipole moments of homogeneous elementar solids Julian Stirling 1,2, and Stephan Schlamminger 1 1 National Institute of Standards and Technolog, 1 Bureau
More information4 Strain true strain engineering strain plane strain strain transformation formulae
4 Strain The concept of strain is introduced in this Chapter. The approimation to the true strain of the engineering strain is discussed. The practical case of two dimensional plane strain is discussed,
More informationy R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are:
Curved beams. Introduction Curved beams also called arches were invented about ears ago. he purpose was to form such a structure that would transfer loads, mainl the dead weight, to the ground b the elements
More informationFinite elements for plates and shells. Advanced Design for Mechanical System LEC 2008/11/04
Finite elements for plates and shells Sstem LEC 008/11/04 1 Plates and shells A Midplane The mid-surface of a plate is plane, a curved geometr make it a shell The thickness is constant. Ma be isotropic,
More informationTheory of Elasticity Formulation of the Mindlin Plate Equations
Theor of lasticit Formulation of the indlin Plate quations Nwoji, C.U. #1, Onah H.N. #, ama B.O. #3, Ike, C.C. * 4 #1, #, #3 Dept of Civil ngineering, Universit of Nigeria, Nsukka, nugu State, Nigeria.
More informationBending Analysis of Isotropic Rectangular Plate with All Edges Clamped: Variational Symbolic Solution
Journal of Emerging Trends in Engineering and pplied Sciences (JETES) (5): 86-85 Scholarlink Research Institute Journals, 0 (ISSN: -706) jeteas.scholarlinkresearch.org Journal of Emerging Trends in Engineering
More informationMAE 323: Chapter 4. Plane Stress and Plane Strain. The Stress Equilibrium Equation
The Stress Equilibrium Equation As we mentioned in Chapter 2, using the Galerkin formulation and a choice of shape functions, we can derive a discretized form of most differential equations. In Structural
More informationARTICLE IN PRESS. Thin-Walled Structures
RTICLE I PRESS Thin-Walled Structures 47 () 4 4 Contents lists availale at ScienceDirect Thin-Walled Structures journal homepage: www.elsevier.com/locate/tws Buckling analsis of plates using the two variale
More informationMultiple Integration
Contents 7 Multiple Integration 7. Introduction to Surface Integrals 7. Multiple Integrals over Non-rectangular Regions 7. Volume Integrals 4 7.4 Changing Coordinates 66 Learning outcomes In this Workbook
More informationVibration Power Transmission Through Multi-Dimensional Isolation Paths over High Frequencies
001-01-145 Vibration ower ransmission hrough Multi-Dimensional Isolation aths over High Frequencies Copright 001 Societ of Automotive Engineers, Inc. Seungbo im and Rajendra Singh he Ohio State Universit
More information16.5. Maclaurin and Taylor Series. Introduction. Prerequisites. Learning Outcomes
Maclaurin and Talor Series 6.5 Introduction In this Section we eamine how functions ma be epressed in terms of power series. This is an etremel useful wa of epressing a function since (as we shall see)
More informationBending Analysis of Symmetrically Laminated Plates
Leonardo Journal of Sciences ISSN 1583-0233 Issue 16, January-June 2010 p. 105-116 Bending Analysis of Symmetrically Laminated Plates Bouazza MOKHTAR 1, Hammadi FODIL 2 and Khadir MOSTAPHA 2 1 Department
More informationME 7502 Lecture 2 Effective Properties of Particulate and Unidirectional Composites
ME 75 Lecture Effective Properties of Particulate and Unidirectional Composites Concepts from Elasticit Theor Statistical Homogeneit, Representative Volume Element, Composite Material Effective Stress-
More informationCitation Key Engineering Materials, ,
NASITE: Nagasaki Universit's Ac Title Author(s) Interference Analsis between Crack Plate b Bod Force Method Ino, Takuichiro; Ueno, Shohei; Saim Citation Ke Engineering Materials, 577-578, Issue Date 2014
More informationStability Analysis of Laminated Composite Thin-Walled Beam Structures
Paper 224 Civil-Comp Press, 2012 Proceedings of the Eleventh International Conference on Computational Structures echnolog, B.H.V. opping, (Editor), Civil-Comp Press, Stirlingshire, Scotland Stabilit nalsis
More information7.4 The Elementary Beam Theory
7.4 The Elementary Beam Theory In this section, problems involving long and slender beams are addressed. s with pressure vessels, the geometry of the beam, and the specific type of loading which will be
More informationStructural Dynamics Lecture Eleven: Dynamic Response of MDOF Systems: (Chapter 11) By: H. Ahmadian
Structural Dynamics Lecture Eleven: Dynamic Response of MDOF Systems: (Chapter 11) By: H. Ahmadian ahmadian@iust.ac.ir Dynamic Response of MDOF Systems: Mode-Superposition Method Mode-Superposition Method:
More informationEFFECT OF DAMPING AND THERMAL GRADIENT ON VIBRATIONS OF ORTHOTROPIC RECTANGULAR PLATE OF VARIABLE THICKNESS
Available at http://pvamu.edu/aam Appl. Appl. Math. ISSN: 193-9466 Vol. 1, Issue 1 (June 17), pp. 1-16 Applications and Applied Mathematics: An International Journal (AAM) EFFECT OF DAMPING AND THERMAL
More informationNonlinear dynamic response of a simply supported rectangular functionally graded material plate under the time-dependent thermalmechanical loads
Journal of Mechanical Science and echnolog 5 (7 (11 167~1646 www.springerlink.com/content/178-494 DOI 1.17/s16-11-51-1 Nonlinear dnamic response of a simpl supported rectangular functionall graded material
More informationOn the Extension of Goal-Oriented Error Estimation and Hierarchical Modeling to Discrete Lattice Models
On the Etension of Goal-Oriented Error Estimation and Hierarchical Modeling to Discrete Lattice Models J. T. Oden, S. Prudhomme, and P. Bauman Institute for Computational Engineering and Sciences The Universit
More informationANALYSIS OF BI-STABILITY AND RESIDUAL STRESS RELAXATION IN HYBRID UNSYMMETRIC LAMINATES
ANALYSIS OF BI-STABILITY AND RESIDUAL STRESS RELAXATION IN HYBRID UNSYMMETRIC LAMINATES Fuhong Dai*, Hao Li, Shani Du Center for Composite Material and Structure, Harbin Institute of Technolog, China,5
More informationLongitudinal buckling of slender pressurised tubes
Fluid Structure Interaction VII 133 Longitudinal buckling of slender pressurised tubes S. Syngellakis Wesse Institute of Technology, UK Abstract This paper is concerned with Euler buckling of long slender
More informationMECHANICS OF MATERIALS REVIEW
MCHANICS OF MATRIALS RVIW Notation: - normal stress (psi or Pa) - shear stress (psi or Pa) - normal strain (in/in or m/m) - shearing strain (in/in or m/m) I - area moment of inertia (in 4 or m 4 ) J -
More informationKirchhoff Plates: Field Equations
20 Kirchhoff Plates: Field Equations AFEM Ch 20 Slide 1 Plate Structures A plate is a three dimensional bod characterized b Thinness: one of the plate dimensions, the thickness, is much smaller than the
More informationURL: <http://dx.doi.org/ / >
Citation: Thai, Huu-Tai, Vo, Thuc, Nguen, Trung-Kien and Lee, Jaehong (14) A nonlocal sinusoidal plate model for micro/nanoscale plates. Proceedings of the Institution of Mechanical Engineers, Part C:
More informationMMJ1153 COMPUTATIONAL METHOD IN SOLID MECHANICS PRELIMINARIES TO FEM
B Course Content: A INTRODUCTION AND OVERVIEW Numerical method and Computer-Aided Engineering; Phsical problems; Mathematical models; Finite element method;. B Elements and nodes, natural coordinates,
More informationStability Analysis of a Geometrically Imperfect Structure using a Random Field Model
Stabilit Analsis of a Geometricall Imperfect Structure using a Random Field Model JAN VALEŠ, ZDENĚK KALA Department of Structural Mechanics Brno Universit of Technolog, Facult of Civil Engineering Veveří
More information2766. Differential quadrature method (DQM) for studying initial imperfection effects and pre- and post-buckling vibration of plates
2766. Differential quadrature method (DQM) for studying initial imperfection effects and pre- and post-buckling vibration of plates Hesam Makvandi 1, Shapour Moradi 2, Davood Poorveis 3, Kourosh Heidari
More informationTHE GENERAL ELASTICITY PROBLEM IN SOLIDS
Chapter 10 TH GNRAL LASTICITY PROBLM IN SOLIDS In Chapters 3-5 and 8-9, we have developed equilibrium, kinematic and constitutive equations for a general three-dimensional elastic deformable solid bod.
More informationFree vibration analysis of beams by using a third-order shear deformation theory
Sādhanā Vol. 32, Part 3, June 2007, pp. 167 179. Printed in India Free vibration analysis of beams by using a third-order shear deformation theory MESUT ŞİMŞEK and TURGUT KOCTÜRK Department of Civil Engineering,
More informationBOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS
BOUNDARY EFFECTS IN STEEL MOMENT CONNECTIONS Koung-Heog LEE 1, Subhash C GOEL 2 And Bozidar STOJADINOVIC 3 SUMMARY Full restrained beam-to-column connections in steel moment resisting frames have been
More informationx y plane is the plane in which the stresses act, yy xy xy Figure 3.5.1: non-zero stress components acting in the x y plane
3.5 Plane Stress This section is concerned with a special two-dimensional state of stress called plane stress. It is important for two reasons: () it arises in real components (particularl in thin components
More informationThe Plane Stress Problem
. 4 The Plane Stress Problem 4 Chapter 4: THE PLANE STRESS PROBLEM 4 TABLE OF CONTENTS Page 4.. INTRODUCTION 4 3 4... Plate in Plane Stress............... 4 3 4... Mathematical Model.............. 4 4
More informationNATURAL FREQUENCIES OF A HONEYCOMB SANDWICH PLATE Revision F. A diagram of a honeycomb plate cross-section is shown in Figure 1.
NATURAL FREQUENCIES OF A HONEYCOMB SANDWICH PLATE Revision F By Tom Irvine Email: tomirvine@aol.com August 5, 008 Bending Stiffness of a Honeycomb Sandwich Plate A diagram of a honeycomb plate cross-section
More informationTHE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY. V. A. Sharifulin.
THE HEATED LAMINAR VERTICAL JET IN A LIQUID WITH POWER-LAW TEMPERATURE DEPENDENCE OF DENSITY 1. Introduction V. A. Sharifulin Perm State Technical Universit, Perm, Russia e-mail: sharifulin@perm.ru Water
More informationSEPARABLE EQUATIONS 2.2
46 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 4. Chemical Reactions When certain kinds of chemicals are combined, the rate at which the new compound is formed is modeled b the autonomous differential equation
More informationStiffness and Strength Tailoring in Uniform Space-Filling Truss Structures
NASA Technical Paper 3210 April 1992 Stiffness and Strength Tailoring in Uniform Space-Filling Truss Structures Mark S. Lake Summar This paper presents a deterministic procedure for tailoring the continuum
More informationc 1999 Society for Industrial and Applied Mathematics
SIAM J. SCI. COMPUT. Vol., No. 6, pp. 978 994 c 999 Societ for Industrial and Applied Mathematics A STUDY OF MONITOR FUNCTIONS FOR TWO-DIMENSIONAL ADAPTIVE MESH GENERATION WEIMING CAO, WEIZHANG HUANG,
More informationWave Phenomena Physics 15c
Wave Phenomena Phsics 15c Lecture 13 Multi-Dimensional Waves (H&L Chapter 7) Term Paper Topics! Have ou found a topic for the paper?! 2/3 of the class have, or have scheduled a meeting with me! If ou haven
More information2.2 SEPARABLE VARIABLES
44 CHAPTER FIRST-ORDER DIFFERENTIAL EQUATIONS 6 Consider the autonomous DE 6 Use our ideas from Problem 5 to find intervals on the -ais for which solution curves are concave up and intervals for which
More informationGeometric Stiffness Effects in 2D and 3D Frames
Geometric Stiffness Effects in D and 3D Frames CEE 41. Matrix Structural Analsis Department of Civil and Environmental Engineering Duke Universit Henri Gavin Fall, 1 In situations in which deformations
More informationCOPYRIGHTED MATERIAL. Index
Index A Admissible function, 163 Amplification factor, 36 Amplitude, 1, 22 Amplitude-modulated carrier, 630 Amplitude ratio, 36 Antinodes, 612 Approximate analytical methods, 647 Assumed modes method,
More informationCorrection of local-linear elasticity for nonlocal residuals: Application to Euler-Bernoulli beams
Correction of local-linear elasticity for nonlocal residuals: Application to Euler-Bernoulli beams Mohamed Shaat* Engineering and Manufacturing Technologies Department, DACC, New Mexico State University,
More informationThree-dimensional free vibration analysis of functionally graded rectangular plates using the B-spline Ritz method
The 01 World Congress on Advances in Civil, Environmental, and Materials Research (ACEM 1) Seoul, Korea, August 6-30, 01 Three-dimensional free viration analsis of functionall graded rectangular plates
More informationCOMPACT IMPLICIT INTEGRATION FACTOR METHODS FOR A FAMILY OF SEMILINEAR FOURTH-ORDER PARABOLIC EQUATIONS. Lili Ju. Xinfeng Liu.
DISCRETE AND CONTINUOUS doi:13934/dcdsb214191667 DYNAMICAL SYSTEMS SERIES B Volume 19, Number 6, August 214 pp 1667 1687 COMPACT IMPLICIT INTEGRATION FACTOR METHODS FOR A FAMILY OF SEMILINEAR FOURTH-ORDER
More informationWave Phenomena Physics 15c
Wave Phenomena Phsics 15c Lecture 13 Multi-Dimensional Waves (H&L Chapter 7) Term Paper Topics! Have ou found a topic for the paper?! 2/3 of the class have, or have scheduled a meeting with me! If ou haven
More informationKirchhoff Plates: Field Equations
20 Kirchhoff Plates: Field Equations 20 1 Chapter 20: KIRCHHOFF PLATES: FIELD EQUATIONS TABLE OF CONTENTS Page 20.1 Introduction..................... 20 3 20.2 Plates: Basic Concepts................. 20
More informationConsider a slender rod, fixed at one end and stretched, as illustrated in Fig ; the original position of the rod is shown dotted.
4.1 Strain If an object is placed on a table and then the table is moved, each material particle moves in space. The particles undergo a displacement. The particles have moved in space as a rigid bod.
More informationSolving Variable-Coefficient Fourth-Order ODEs with Polynomial Nonlinearity by Symmetric Homotopy Method
Applied and Computational Mathematics 218; 7(2): 58-7 http://www.sciencepublishinggroup.com/j/acm doi: 1.11648/j.acm.21872.14 ISSN: 2328-565 (Print); ISSN: 2328-5613 (Online) Solving Variable-Coefficient
More informationTable of Contents. Preface... 13
Table of Contents Preface... 13 Chapter 1. Vibrations of Continuous Elastic Solid Media... 17 1.1. Objective of the chapter... 17 1.2. Equations of motion and boundary conditions of continuous media...
More informationEVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING
EVALUATION OF STRESS IN BMI-CARBON FIBER LAMINATE TO DETERMINE THE ONSET OF MICROCRACKING A Thesis b BRENT DURRELL PICKLE Submitted to the Office of Graduate Studies of Teas A&M Universit in partial fulfillment
More informationTime-Frequency Analysis: Fourier Transforms and Wavelets
Chapter 4 Time-Frequenc Analsis: Fourier Transforms and Wavelets 4. Basics of Fourier Series 4.. Introduction Joseph Fourier (768-83) who gave his name to Fourier series, was not the first to use Fourier
More informationDynamics of multiple pendula without gravity
Chaotic Modeling and Simulation (CMSIM) 1: 57 67, 014 Dnamics of multiple pendula without gravit Wojciech Szumiński Institute of Phsics, Universit of Zielona Góra, Poland (E-mail: uz88szuminski@gmail.com)
More informationAn efficient analytical model to evaluate the first two local buckling modes of finite cracked plate under tension
278 An efficient analytical model to evaluate the first two local buckling modes of finite cracked plate under tension Abstract The analytical approach is presented for both symmetric and anti-symmetric
More informationResearch Article Equivalent Elastic Modulus of Asymmetrical Honeycomb
International Scholarl Research Network ISRN Mechanical Engineering Volume, Article ID 57, pages doi:.5//57 Research Article Equivalent Elastic Modulus of Asmmetrical Honecomb Dai-Heng Chen and Kenichi
More informationAnalytical Strip Method for Thin Isotropic Cylindrical Shells
IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE) e-issn: 2278-1684,p-ISSN: 2320-334X, Volume 14, Issue 4 Ver. III (Jul. Aug. 2017), PP 24-38 www.iosrjournals.org Analytical Strip Method for
More informationFIRST- AND SECOND-ORDER IVPS The problem given in (1) is also called an nth-order initial-value problem. For example, Solve: Solve:
.2 INITIAL-VALUE PROBLEMS 3.2 INITIAL-VALUE PROBLEMS REVIEW MATERIAL Normal form of a DE Solution of a DE Famil of solutions INTRODUCTION We are often interested in problems in which we seek a solution
More informationINTERFACE CRACK IN ORTHOTROPIC KIRCHHOFF PLATES
Gépészet Budapest 4-5.Ma. G--Section-o ITERFACE CRACK I ORTHOTROPIC KIRCHHOFF PLATES András Szekrénes Budapest Universit of Technolog and Economics Department of Applied Mechanics Budapest Műegetem rkp.
More informationUNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX METHOD
Proceedings of the 3rd ASME/JSME Joint Fluids Engineering Conference Jul 8-23, 999, San Francisco, California FEDSM99-8 UNSTEADY LOW REYNOLDS NUMBER FLOW PAST TWO ROTATING CIRCULAR CYLINDERS BY A VORTEX
More informationTwo-Dimensional Analysis of the Power Transfer between Crossed Laser Beams
Two-Dimensional Analsis of the Power Transfer between Crossed Laser Beams The indirect-drive approach to inertial confinement fusion involves laser beams that cross as the enter the hohlraum. Ionacoustic
More informationCalculus of the Elastic Properties of a Beam Cross-Section
Presented at the COMSOL Conference 2009 Milan Calculus of the Elastic Properties of a Beam Cross-Section Dipartimento di Modellistica per l Ingegneria Università degli Studi della Calabria (Ital) COMSOL
More informationMECHANICS OF MATERIALS
00 The McGraw-Hill Companies, Inc. All rights reserved. T Edition CHAPTER MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Teas Tech Universit
More informationA PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS
1 A PROTOCOL FOR DETERMINATION OF THE ADHESIVE FRACTURE TOUGHNESS OF FLEXIBLE LAMINATES BY PEEL TESTING: FIXED ARM AND T-PEEL METHODS An ESIS Protocol Revised June 2007, Nov 2010 D R Moore, J G Williams
More informationChapter 3: BASIC ELEMENTS. solid mechanics)
Chapter 3: BASIC ELEMENTS Section 3.: Preliminaries (review of solid mechanics) Outline Most structural analsis FE codes are displacement based In this chapter we discuss interpolation methods and elements
More informationA NEW REFINED THEORY OF PLATES WITH TRANSVERSE SHEAR DEFORMATION FOR MODERATELY THICK AND THICK PLATES
A NEW REFINED THEORY OF PLATES WITH TRANSVERSE SHEAR DEFORMATION FOR MODERATELY THICK AND THICK PLATES J.M. MARTÍNEZ VALLE Mechanics Department, EPS; Leonardo da Vinci Building, Rabanales Campus, Cordoba
More informationKINEMATIC RELATIONS IN DEFORMATION OF SOLIDS
Chapter 8 KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS Figure 8.1: 195 196 CHAPTER 8. KINEMATIC RELATIONS IN DEFORMATION OF SOLIDS 8.1 Motivation In Chapter 3, the conservation of linear momentum for a
More informationMechanics of Materials and Structures
Journal of Mechanics of Materials and Structures VIBRATION CHARACTERISTICS OF CURVED BEAMS Chong-Seok Chang and Dewey H. Hodges Volume 4, Nº 4 April 9 mathematical sciences publishers JOURNAL OF MECHANICS
More informationFunctions of Several Variables
Chapter 1 Functions of Several Variables 1.1 Introduction A real valued function of n variables is a function f : R, where the domain is a subset of R n. So: for each ( 1,,..., n ) in, the value of f is
More informationFluid Mechanics II. Newton s second law applied to a control volume
Fluid Mechanics II Stead flow momentum equation Newton s second law applied to a control volume Fluids, either in a static or dnamic motion state, impose forces on immersed bodies and confining boundaries.
More informationCONTINUOUS SPATIAL DATA ANALYSIS
CONTINUOUS SPATIAL DATA ANALSIS 1. Overview of Spatial Stochastic Processes The ke difference between continuous spatial data and point patterns is that there is now assumed to be a meaningful value, s
More informationTime-Frequency Analysis: Fourier Transforms and Wavelets
Chapter 4 Time-Frequenc Analsis: Fourier Transforms and Wavelets 4. Basics of Fourier Series 4.. Introduction Joseph Fourier (768-83) who gave his name to Fourier series, was not the first to use Fourier
More information4.7. Newton s Method. Procedure for Newton s Method HISTORICAL BIOGRAPHY
4. Newton s Method 99 4. Newton s Method HISTORICAL BIOGRAPHY Niels Henrik Abel (18 189) One of the basic problems of mathematics is solving equations. Using the quadratic root formula, we know how to
More informationN coupled oscillators
Waves 1 1 Waves 1 1. N coupled oscillators towards the continuous limit. Stretched string and the wave equation 3. The d Alembert solution 4. Sinusoidal waves, wave characteristics and notation T 1 T N
More informationSimulation of Acoustic and Vibro-Acoustic Problems in LS-DYNA using Boundary Element Method
10 th International LS-DYNA Users Conference Simulation Technolog (2) Simulation of Acoustic and Vibro-Acoustic Problems in LS-DYNA using Boundar Element Method Yun Huang Livermore Software Technolog Corporation
More informationChapter 11 Three-Dimensional Stress Analysis. Chapter 11 Three-Dimensional Stress Analysis
CIVL 7/87 Chapter - /39 Chapter Learning Objectives To introduce concepts of three-dimensional stress and strain. To develop the tetrahedral solid-element stiffness matri. To describe how bod and surface
More informationChapter 2 Overview of the Simulation Methodology
Chapter Overview of the Simulation Methodolog. Introduction This chapter presents an overview of the simulation methodolog that comprises both the art and science involved in simulating phsical phenomena.
More informationEffect of plate s parameters on vibration of isotropic tapered rectangular plate with different boundary conditions
Original Article Effect of plate s parameters on vibration of isotropic tapered rectangular plate ith different boundar conditions Journal of Lo Frequenc Noise, Vibration and Active Control 216, Vol. 35(2)
More information