Three-dimensional free vibration analysis of functionally graded rectangular plates using the B-spline Ritz method
|
|
- Arron Rogers
- 5 years ago
- Views:
Transcription
1 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 using the B-spline Rit method *Harunou Nagino 1), Motohiro Sato ), Tomisaku Miusawa 3) and Takashi Mikami 4) 1) Department of Civil and Environmental Engineering, Oita National College of Technolog, 1666 Maki, Oita , Japan ) Division of Engineering and Polic for Sustainale Environment, Facult of Engineering, Hokkaido Universit, Kita 13 Nishi 8, Kita-ku, Sapporo , Japan 3) Civil Engineering and Environmental Design Course, Daido Universit, Hakusui-cho 40, Minami-ku, Nagoa , Japan 4) Hokkaido Universit, Kita 13 Nishi 8, Kita-ku, Sapporo , Japan 1) nagino@oita-ct.ac.jp ABSTRACT This paper presents the three-dimensional free viration analsis of functionall graded rectangular plates with aritrar oundar conditions using the B-spline Rit method ased on the theor of elasticit. The Young s modulus of the plate is assumed to var through the thickness direction, and the Poisson s ratio and densit are constant. The convergence and accurac of the present method were investigated. Rapid, stale convergence and high accurac were otained the present method. Furthermore, the effects of thickness-to-length ratio, Young s modulus ratio and oundar condition on the fundamental frequenc parameters, mode shapes, strain energies and kinetic energies of functionall graded plate were also carried out. 1. INTRODUCTION Functionall graded materials (FGMs) were first proposed a group of Japanese material scientists (Koiumi 1997). The material propert of FGMs varies smoothl and continuousl through the thickness from the surface to other surface. FGMs have received considerale attention in modern technolog as a structural element or a material ingredient due to increasing performance demands, and are epected as a future high performance composite material in man engineering fields as aerospace, nuclear, marine, and civil engineering, etc. Therefore, an understanding of the dnamic ehavior of the structure memers made of FGMs is ver important in structural design. 1), ) Associate Professor, 3) Professor, 4) Vice President
2 The free viration analsis of structural memers ased on the three-dimensional (3-D) theor of elasticit does not rel to hpotheses involving kinematics of deformation. Therefore, 3-D free viration analsis provides realistic results ased on the theor, and it can not e predicted shear deformation theories (Mindlin 1951, Redd 1985). The studies on the 3-D free virations of rectangular plates made of FGMs are limited to four edges simpl-supported condition (Vel 004). Recentl, Malekadeh (009) proposed the semi-analtical differential quadrature method, and analed 3-D free virations of functionall graded rectangular plates with one pair of parallel simpl-supported edges. This paper presents the 3-D free viration analsis of functionall graded rectangular plates with aritrar oundar conditions using the B-spline Rit method. The Young s modulus of the plate is assumed to var through the thickness direction, and the Poisson s ratio and densit are constant. The analsis is ased on the linear, small-deformation 3-D theor of elasticit. The B-spline Rit method has een proposed Nagino (008). This method is formulated the Rit procedure with triplicate series of normalied B-spline functions (Boor 197) as displacement amplitude components. The geometric oundar conditions are numericall satisfied the method of artificial spring (Kao 1974). To demonstrate the convergence and accurac of the present method, several eamples are solved, and the results are compared with the 3-D finite element solutions. Furthermore, a detailed investigation of the effects of thickness-to-length ratio, Young s modulus ratio and oundar condition on the fundamental frequenc parameters, mode shapes, strain energies and kinetic energies of functionall graded plate are also carried out.. FORMULATION.1. Material properties of FGMs The Young s modulus E( ) in the functionall graded plate is assumed to var eponentiall in the thickness direction as follows: where E t and E ( ) = E ep p h, ln E t p =, (1) E E are the Young s moduli at top and ottom surface, respectivel. Poisson s ratio ν and densit ρ are constant. The distriution of Young s modulus E( ) in the thickness direction is shown in Fig Analtical model Consider a functionall graded rectangular plate with length a, width and uniform thickness h in Fig.. The stress free surface are assumed at = 0 and =h. The plate is defined with respect to a right-handed orthogonal coordinate sstem (,, ). The periodic displacement components at an point are defined the in-plane components u, v and the transverse component w in the, and direction, respectivel.
3 1.00 / h E t / E = 10 E t / E = 5 E t / E = 1 E t / E = 1 / 5 E t / E = 1 / E () Fig. 1. The distriution of Young s modulus in the thickness direction, v, w h O a E t E Fig.. Coordinate sstem and geometr of functionall graded plate, u.3. Formulation of eigenvalue equation ased on the B-spline Rit method The strain energ U of the functionall graded rectangular plate can e epressed in integral form as U 1 a h = ( )d d d σε σε + σε + τγ + τ γ + τγ, () in which ε, ε, ε, γ, γ, γ and σ, σ, σ, τ, τ, τ are strain and stress components, respectivel. In the 3-D theor of elasticit, strain and stress components of the functionall graded rectangular plate are defined as u ε =, ε v w =, ε =, γ u v = +, γ v w = +, γ w u = +, (3)
4 σ = { µ ( ) + G ( )} ε + µ ( ) ε + µ ( ) ε, σ = µ () ε + {() µ + G()} ε + µ () ε, σ = µ ( ) ε + µ ( ) ε + { µ ( ) + G( )} ε, τ = G ( ) γ, τ = G ( ) γ, τ = G ( ) γ, (4) ν E ( ) µ ( ) =, (1 ν )(1 + ν ) E( ) G ( ) =, (5) (1 + ν ) where E( ) is Young s modulus, ν is Poisson s ratio, and G ( ) is shear modulus. The kinetic energ T of the plate can e written as T ρ a h u v w = ddd t t t, (6) in which ρ is the mass densit per unit volume. Here, for simplicit and convenience in mathematical formulation, the following nondimensional coordinate sstem (ξ, η, ζ ) are introduced as ξ =, a η =, ζ =. (7) h The periodic displacement components can e epressed non-dimensional displacement amplitude function U, V and W in ξ, η and ζ coordinates and the temporal coordinate t as i u( ξηζ,,, t) au( ξηζ,, ) e ωt =, i v( ξηζ,,, t) av( ξηζ,, ) e ωt =, i w( ξηζ,,, t) aw( ξηζ,, ) e ωt =, (8) where ω denotes the circular frequenc and i = 1 is an imaginar constant. The assumed spatial displacement field is ased on a separale assumption for displacement amplitude functions. The functions are epressed as the summation of a triplicate series of B-spline functions as follows: iξ iη iζ U( ξ, η, ζ ) A N ( ξ) N ( η) N ( ζ ) =, m= 1 n= 1 r= 1 iξ iη iζ m= 1 n= 1 r= 1 mnr m, kξ n, kη r, kζ V( ξ, η, ζ ) B N ( ξ) N ( η) N ( ζ ) =, iξ iη iζ m= 1 n= 1 r= 1 mnr m, kξ n, kη r, kζ W( ξ, η, ζ ) = C N ( ξ) N ( η) N ( ζ ), (9) mnr m, kξ n, kη r, kζ
5 in which N m, k ξ ( ξ ), N n, k η ( η) and N r, k ζ ( ζ ) are one-dimensional (1-D) normalied B- spline functions with the degree of spline function ( k ξ 1), ( k η 1) and ( k ζ 1). A mnr, B mnr and C mnr are unknown spline coefficients. The appearing in Eq. (9) are defined as: i k = mξ + kξ, i k = mη + kη and i k = mζ + kζ, where m ξ, m η, m ζ and k ξ, k η, ξ η ζ kζ are the numer of knots and the order of spline function in the ξ, η and ζ directions, respectivel. Sustituting Eqs. (7), (8) and (9) into Eqs. () and (6), the maimum strain energ U ma and maimum kinetic energ T ma of the plate can e written in a non-dimensional coordinate sstems as ahe U ( )d d d ma = σ ε + σ ε + σε + τγ + τ γ + τ γ ζ η ξ ahe T = { } [K P ]{ }, (10) 3 ah Tma = ρω ( U + V + W )d ζ d η d ξ ρω ah T = { } [M]{ }, (11) where [K P ] and [M] are the stiffness and mass matrices of the plate, respectivel, and { } is unknown coefficient vector in the following: { δ δ δ } T { } = { } { } { }, (1) A B C in which the column vectors { δ A }, { δ B } and { δ C } as { } { } T δ A = A111 A11 A11 i A11 A1 i A1 i i A ζ ζ η ζ iξ iηi, ζ { } { } T δ B = B111 B11 B11 i B11 B1 i B1 i i B ζ ζ η ζ iξ iηi, ζ { } { } T δ C = C111 C11 C11 i C11 C1 i C1 i i C ζ ζ η ζ iξ iηi. (13) ζ The oundar conditions at the four edges ( = 0, a and = 0, ) of a functionall graded rectangular plate would e satisfied as follows: Simpl supported: v = w = 0, σ = 0 at ( = 0, a), u = w = 0, σ = 0 at ( = 0, ). (14)
6 Clamped edge: u = v = w = 0 at ( = 0, a), u = v = w = 0 at ( = 0, ). (15) Free edge: σ = τ = τ = 0 at ( = 0, a), σ = τ = τ = 0 at ( = 0, ). (16) The oundar conditions for top and ottom stress free surfaces of the plate can e epressed σ = τ = τ = 0 at ( = 0, h). (17) To deal with the geometric oundar conditions at the four edges ( = 0, a and = 0, ), the method of artificial spring (Kao 1974) is used. In this method, three tpes of spring coefficient α, β and γ corresponding to the geometric oundar conditions u, v, w are introduced at each oundar edges of the plate. The energ contriution L due to the spring is given 1 1 L= u + v + w + u + v + w h a h ( α β γ )d d ( α β γ )d d = 0, a = 0,. (18) Sustituting Eqs. (7), (8) and (9) into Eq. (18), the maimum artificial spring energ L of the plate can e given in a non-dimensional coordinate sstems as ma 3 ah ah Lma = ( αu βv γw )dζ d η ( αu βv γw )dζ dξ ξ= 0,1 η= 0,1 ahe T = { } [K L]{ }, (19) where [K L] is the stiffness matri for the artificial springs. For the geometric oundar condition at the four edges (ξ = 0, 1 and η = 0, 1), the non-dimensional spring parameters are assumed to e ero, the oundar edges will ecome the stress free condition. If the spring parameter is assumed to e infinite, the oundar edges will lead to procedure the clamped condition. The total potential energ Π of the functionall graded plate can e epressed as Π= ( U + L ) T. (0) ma ma ma In Eq. (0), minimiing the total potential energ Π with respect to the unknown spline coefficient vector { } i.e.:
7 Π = 0, (1) { } which lead to the following the eigenvalue equation in matri form: [K UU ] [K UV] [K UW ] [M UU ] [0] [0] { δ A} {0} [K VU] [K VV ] [K VW ] [0] [M VV] [0] Ω { δ B} = {0}, () [K WU ] [K WV ] [K WW ] [0] [0] [M WW ] { δc} {0} Ω = ω, (3) a E ρ where Ω is the non-dimensional frequenc parameter, [K IJ ] and [M IJ ] (I, J = U, V, W) are the su-stiffness matrices and su-mass matrices of the plate, respectivel. The sie of matri in Eq. () is 3( m k )( m + k )( m + k ). 3. NUMERICAL RESULTS ξ + ξ η η ζ ζ The fundamental natural frequencies of the functionall graded rectangular plates with aritrar oundar conditions were analed. Firstl, the convergence and accurac of the present method were investigated. Net, the effects of thickness-tolength ratio h / a, Young s modulus ratio E t / E and oundar condition on the fundamental frequenc parameters, mode shapes, strain energies and kinetic energies of functionall graded plate were also carried out. Poisson s ration ν = 0.3 and aspect ratio / a = 1 were used in the numerical calculations. For the definition of the oundar conditions of the plate, for eample, the smols SF-CS, identifies a plate with edges (ξ = 0, 1) and (η = 0, 1) having simpl supported edge (S), free edge (F), clamped edge (C) and simpl supported edge (S), respectivel. The non-dimensional 8 artificial spring parameters are used to e 10 and the placement of the knots was set to the Cheshev-Gauss-Loatto points, namel, the shifted Cheshev points (Nagino 008) in the following analsis. All computations are performed in doule precision on a personal computer, and all of the fundamental frequenc parameter Ω 1st = ω 1st a ρ / E and viration modes are organied to four significant digits Convergence and comparison studies The Rit method provides theoreticall accurate solutions, and, generall, the natural frequencies otained the Rit procedure are the upper ounds of the eact frequencies. The effects of the degree of spline function (k ξ 1) (k η 1) (k ζ 1) and the numer of knot m ξ m η m ζ on the convergence of the present method are investigated. Moreover, the accurac of the present method is also investigated.
8 Tale 1. Convergence of fundamental frequenc parameter Ω 1st for SS-SS functionall graded plates: E / E = 100 t h / a ( kξ 1) ( kη 1) ( kζ 1) mξ mη mζ D.O.F. Ω 1st (Error %) D FEM (C3D8) ( 0.63 %) ( 0.7 %) D FEM (C3D8) ( 0.09 %) ( 0.03 %) Tale. Convergence of fundamental frequenc parameter functionall graded plates: E / E = 100 t Ω 1st for CC-CC h / a ( kξ 1) ( kη 1) ( kζ 1) mξ mη mζ D.O.F. Ω 1st (Error %) D FEM (C3D8) ( 0.40 %) ( 0.15 %) D FEM (C3D8) ( %) ( %)
9 Tale 3. Convergence of fundamental frequenc parameter Ω 1st for CF-FF functionall graded plates: E / E = 100 t h / a ( kξ 1) ( kη 1) ( kζ 1) mξ mη mζ D.O.F. Ω 1st (Error %) D FEM (C3D8) ( 0.1 %) ( 0.06 %) D FEM (C3D8) ( %) ( %) Tales 1, and 3 show the effects of the degree of spline function (k ξ 1) (k η 1) (k ζ 1) and the numer of knot m ξ m η m ζ on the convergence of the fundamental frequenc parameter Ω 1st for functionall graded square plate having SS-SS, CC-CC and CF-FF respectivel. The thickness-to-length ratio h / a are set as 0. (moderatel thick plate) and 0.5 (thick plate), and the Young s modulus ratio E t / E = 100 is used. The results are compared with the 3-D finite element solutions Aaqus 6.1. Here, C3D8 means first-order solid element. The error (%) is defined as follows: Ω Ω FEM Present Error (%) = 100 ΩPresent, (4) where Ω Present is convergence value otained from present method in Tales 1, and 3. Tales 1, and 3 show that stale convergence can e otained. It is found that the fundamental frequenc parameter Ω 1st rapidl converge using the degree of spline function The results in Tales 1, and 3 show ecellent agreements in all cases; thus, high accurac is otained. The B-spline Rit method ields highl accurate results with few degrees of freedom (D.O.F.) for the fundamental frequencies and displacement mode shapes of the functionall graded rectangular plate. In addition, stale and rapidl converging and ecellent upper ound solutions are otained the present method regardless of the thickness-to-length ratio and oundar conditions.
10 Ω 1st E t / E = 100 E t / E = 10 E t / E = 1 E t / E = 1/10 E t / E = 1/100 Ω 1st (FGM) / Ω 1st (Isotropic) E t / E = 100 E t / E = 10 E t / E = 1 E t / E = 1/10 E t / E = 1/ h / a (a) h / a Ω 1st () Ω1st (FGM) / Ω 1st (Isotropic) Fig. 3. The effects of thickness-to-length ratio and Young s modulus ratio on the fundamental frequenc parameter of CC-CC functionall graded square plates. (a) E t / E = 1 / 10, h / a = 0.1 () E t / E = 1, h / a = 0.1 (c) E t / E = 10, h / a = 0.1 (d) E t / E = 1 / 10, h / a = 0.3 (e) E t / E = 1, h / a = 0.3 (f) E t / E = 10, h / a = 0.3 Fig. 4. The fundamental modes of CC-CC functionall graded square plates. 3.. Results and discussions The B-spline Rit method is applied to investigate the fundamental free viration of the functionall graded square plate with aritrar oundar conditions. Fig. 3 shows the effects of thickness-to-length ratio h / a and Young s modulus ratio E t / E on the fundamental frequenc parameter Ω 1st of CC-CC functionall graded
11 E t / E = 100 E t / E = 10 E t / E = 1 E t / E = 1/10 E t / E = 1/100 U 0.4 E t / E = 100 E t / E = 10 E 0. t / E = 1 E t / E = 1/10 E t / E = 1/ h / a (a) Bending component U s h / a () Transverse shear component Fig. 5. The effects of thickness-to-length ratio and Young s modulus ratio on the strain energies of fundamental mode for CC-CC functionall graded square plates E t / E = 100 E t / E = 10 E t / E = 1 E t / E = 1/10 E t / E = 1/ T In h / a (a) In-plane component T Trans 0.4 E t / E = 100 E t / E = 10 E 0. t / E = 1 E t / E = 1/10 E t / E = 1/ h / a () Transverse-plane component Fig. 6. The effects of thickness-to-length ratio and Young s modulus ratio on the kinetic energies of fundamental mode for CC-CC functionall graded square plates. square plates. In addition, the fundamental modes of CC-CC functionall graded square plates are depicted in Fig.4. The thickness-to-length ratio h / a varies from 0.01 to 0.5. The Young s modulus ratio E t / E is set as 100, 10, 1, 1/10, and 1/100. Note that E t / E = 1 means an isotropic plate. It is found that the fundamental frequencies parameter Ω 1st increases with increment of thickness-to-length ratio h / a and Young s modulus ratio E t / E. Fig. 5 shows the effects of thickness-to-length ratio h / a and Young s modulus ratio E t / E on the strain energies of fundamental viration mode for CC-CC functionall graded square plates. The numerical calculation condition is the same as the Fig. 3. Here, the ending component U and the transverse shear component U s are defined
12 U U 1 a h = ( σε + σε + τ γ )ddd, (5) ( )ddd. (6) a h s = τ γ + τγ It is seen that the ending component U decreases with increment of thickness-tolength ratio h / a, however, the ending component U of functionall graded plates are greater than the ones of isotropic plates. On the other hand, with increasing thicknessto-length ratio h / a, the transverse shear component U s also increases. But, the transverse shear component U s of functionall graded plates are smaller than the ones of isotropic plates. Thus, it seems that functionall graded materials are strong to transverse shear deformation. Fig. 6 depicts the effects of thickness-to-length ratio h / a and Young s modulus ratio E t / E on the kinetic energies of fundamental mode for CC-CC functionall graded square plates. The numerical calculation condition is the same as the Fig. 3. Here, the In-plane component T In and the transverse-plane component T Trans are defined ρω a h ( T )d d d In = u + v, (7) ρω a h TTrans = d d d w (8) It is seen that the In-plane component T In increases with increment of thickness-tolength ratio h / a and Young s modulus ratio E t / E. On the other hand, the transverseplane component T Trans decreases with increment of thickness-to-length ratio h / a and Young s modulus ratio E t / E Ω 1st SS-SS 1 CC-CC CC-FF h / a Fig. 7. The effects of thickness-to-length ratio and oundar condition the fundamental frequenc parameter of functionall graded square plates.
13 (a) h / a = 0.1, SS-SS () h / a = 0.1, CC-CC (c) h / a = 0.1, CC-FF (d) h / a = 0.3, SS-SS (e) h / a = 0.3, CC-CC (f) h / a = 0.3, CC-FF Fig. 8. The fundamental mode shapes of functionall graded thick plates with SS-SS, CC-CC and CC-FF. Fig. 7 shows the effects of thickness-to-length ratio h / a and oundar condition the fundamental frequenc parameter Ω 1st of functionall graded square plates. The thickness-to-length ratio h / a varies from 0.01 to 0.5. The Young s modulus ratio E t / E is set as 10. In addition, Fig.8 depicts the fundamental mode shapes of functionall graded square plates having SS-SS, CC-CC, CC-FF. From Fig. 7, with increasing the thickness-to-length ratio h / a, the fundamental frequencies parameter Ω 1st also increases regardless of the oundar conditions. 4. COCLUSIONS The 3-D free viration analsis of functionall graded rectangular plates with aritrar oundar conditions has een presented. The governing eigenvalue equation is formulated the B-spline Rit method ased on the linear, small-deformation 3-D theor of elasticit. Rapid, stale convergence and high accurac were otained the present method. Furthermore, the effects of thickness-to-length ratio, Young s modulus ratio and oundar condition on the fundamental frequenc parameters, mode shapes, strain energies and kinetic energies of functionall graded plate were also investigated. The fundamental frequencies parameter increases with increment of thickness-tolength ratio and Young s modulus ratio. Therefore, when the top surface sets higher Young s modulus, the functionall graded plates can increase the natural frequenc than the isotropic plates. Moreover, functionall graded materials are strong to
14 transverse shear deformation. Finall, with increasing the thickness-to-length ratio, the fundamental frequencies parameter also increases regardless of the oundar conditions. ACKNOWLEDGMENT This stud was supported the Ministr of Education, Science, Sports and Culture (MEXT), Grant-in-Aid for Young Scientists (B) (No ) and Japan Societ for the Promotion of Science (JSPS), Grant-in-Aid for Young Scientists (A) (No ). REFERENCES Boor, C.D. (197). On calculating with B-spline, Journal of Approimation Theor, Vol. 6, Kao, R. (1974). On the treatment of oundar conditions the method of artificial parameters, International Journal for Numerical Methods in Engineering, Vol. 8, Koiumi, M. (1997). FGM activities in Japan, Composites Part B, Vol. 8, 1-4. Malekadeh, P. (009). Three-dimensional free viration analsis of thick functionall graded plates on elastic foundations, Composite Structures, Vol.89, Mindlin, R.D. (1951). Influence of rotator inertia and shear on fleural motions of isotropic, elastic plates, ASEM Journal of Applied Mechanics, Vol.73, Nagino, H., Mikami, T., Miusawa, T. (008). Three-dimensional free viration analsis of isotropic rectangular plates using the B-spline Rit method,journal of Sound and Viration, Vol.317, Redd, J.N., Phan, N.D. (1985). Stailit and Viration of isotropic, orthotropic and laminated plates according to a high-order shear deformation theor,journal of Sound and Viration, Vol.98, Vel, S.S., Batra, R.C. (004). Three-dimensional eact solution for the viration of functionall graded rectangular plates, Journal of Sound and Viration, Vol.7,
ARTICLE 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 informationVibration 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 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 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 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 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 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 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 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 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 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 informationComposite Structures
Composite Structures () 5 Contents lists availale at ScienceDirect Composite Structures journal homepage: www.elsevier.com/locate/compstruct A two variale refined plate theor for laminated composite plates
More informationModeling of Rebound Phenomenon of a Rigid Ball with Friction and Elastic Effects
American Control Conference Marriott Waterfront, Baltimore, MD, USA June -Jul, WeB8. Modeling of Reound Phenomenon of a Rigid Ball with Friction and Elastic Effects Akira Nakashima, Yuki Ogawa, Yosuke
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 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 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 informationExact Free Vibration of Webs Moving Axially at High Speed
Eact Free Viration of Wes Moving Aially at High Speed S. HATAMI *, M. AZHARI, MM. SAADATPOUR, P. MEMARZADEH *Department of Engineering, Yasouj University, Yasouj Department of Civil Engineering, Isfahan
More informationExact Shape Functions for Timoshenko Beam Element
IOSR Journal of Computer Engineering (IOSR-JCE) e-iss: 78-66,p-ISS: 78-877, Volume 9, Issue, Ver. IV (May - June 7), PP - www.iosrjournals.org Exact Shape Functions for Timoshenko Beam Element Sri Tudjono,
More informationLecture on: 3D Dislocation Dynamics: Numerical Treatment
Tri-La Short Course on Dislocations in in Materials Pleasanton, CA June 8-0, 998 Lecture on: 3D Dislocation Dnamics: Numerical Treatment H.M. Zi, M. hee & J.P. Hirth School of Mechanical and Materials
More informationInternational Journal of Modern Trends in Engineering and Research e-issn No.: , Date: 2-4 July, 2015
International Journal of Modern Trends in Engineering and Research www.ijmter.com e-issn No.:249-9745, Date: 2-4 July, 215 Thermal Post buckling Analysis of Functionally Graded Materials Cylindrical Shell
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 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 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 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 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 informationFinite Element Method in Geotechnical Engineering
Finite Element Method in Geotechnical Engineering Short Course on + Dynamics Boulder, Colorado January 5-8, 2004 Stein Sture Professor of Civil Engineering University of Colorado at Boulder Contents Steps
More informationVariational formulation of the B.V.P. in terms of displacements is. This principle is particularly useful in analyzing large deflection
4-8 CATIGLIANO' THEOREM OF LEAT WORK. Principle of stationar potential energ: Variational formulation of the B.V.P. in terms of displacements is achieved b the principle. This principle is particularl
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 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 informationSection 1: Review of Elasticity
Finite Elements in Elasticit Section : Review of Elasticit Stress & Strain 2 Constitutive Theor 3 Energ Methods Section : Stress and Strain Stress at a point Q : F = lim A 0 A F = lim A 0 A F = lim A 0
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 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 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 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 informationThree-Dimensional Explicit Parallel Finite Element Analysis of Functionally Graded Solids under Impact Loading. Ganesh Anandakumar and Jeong-Ho Kim
Three-Dimensional Eplicit Parallel Finite Element Analsis of Functionall Graded Solids under Impact Loading Ganesh Anandaumar and Jeong-Ho Kim Department of Civil and Environmental Engineering, Universit
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 informationAE/ME 339. K. M. Isaac Professor of Aerospace Engineering. December 21, 2001 topic13_grid_generation 1
AE/ME 339 Professor of Aerospace Engineering December 21, 2001 topic13_grid_generation 1 The basic idea behind grid generation is the creation of the transformation laws between the phsical space and the
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 information4.5 The framework element stiffness matrix
45 The framework element stiffness matri Consider a 1 degree-of-freedom element that is straight prismatic and symmetric about both principal cross-sectional aes For such a section the shear center coincides
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 informationA refined shear deformation theory for bending analysis of isotropic and orthotropic plates under various loading conditions
JOURNAL OF MATERIALS AND ENGINRING STRUCTURES (015) 3 15 3 Research Paper A refined shear deformation theor for bending analsis of isotropic and orthotropic plates under various loading conditions Bharti
More informationOn the Missing Modes When Using the Exact Frequency Relationship between Kirchhoff and Mindlin Plates
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,
More informationMAE4700/5700 Finite Element Analysis for Mechanical and Aerospace Design
MAE4700/5700 Finite Element Analsis for Mechanical and Aerospace Design Cornell Universit, Fall 2009 Nicholas Zabaras Materials Process Design and Control Laborator Sible School of Mechanical and Aerospace
More informationThe Rotating Inhomogeneous Elastic Cylinders of. Variable-Thickness and Density
Applied Mathematics & Information Sciences 23 2008, 237 257 An International Journal c 2008 Dixie W Publishing Corporation, U. S. A. The Rotating Inhomogeneous Elastic Cylinders of Variable-Thickness and
More informationScienceDirect. Analogy of stress singularities analysis between piezoelectric materials and anisotropic materials
Available online at www.sciencedirect.com Scienceirect Procedia Materials Science ( 4 ) 767 77 th European Conference on Fracture (ECF) Analog of stress singularities analsis between piezoelectric materials
More informationTwo-Dimensional Formulation.
Two-Dimensional Formulation mi@seu.edu.cn Outline Introduction( 概论 ) Two vs. Three-Dimensional Problems Plane Strain( 平面应变 ) Plane Stress( 平面应力 ) Boundar Conditions( 边界条件 ) Correspondence between Plane
More informationChapter 1: Differential Form of Basic Equations
MEG 74 Energ and Variational Methods in Mechanics I Brendan J. O Toole, Ph.D. Associate Professor of Mechanical Engineering Howard R. Hghes College of Engineering Universit of Nevada Las Vegas TBE B- (7)
More informationDynamic Analysis of Laminated Composite Plate Structure with Square Cut-Out under Hygrothermal Load
Dynamic Analysis of Laminated Composite Plate Structure with Square Cut-Out under Hygrothermal Load Arun Mukherjee 1, Dr. Sreyashi Das (nee Pal) 2 and Dr. A. Guha Niyogi 3 1 PG student, 2 Asst. Professor,
More information1.1 The Equations of Motion
1.1 The Equations of Motion In Book I, balance of forces and moments acting on an component was enforced in order to ensure that the component was in equilibrium. Here, allowance is made for stresses which
More informationSIMILARITY METHODS IN ELASTO-PLASTIC BEAM BENDING
Similarity methods in elasto-plastic eam ending XIII International Conference on Computational Plasticity Fundamentals and Applications COMPLAS XIII E Oñate, DRJ Owen, D Peric and M Chiumenti (Eds) SIMILARIT
More informationON THE CHARACTERISTICS OF SOFT SOIL INELASTIC DESIGN RESPONSE SPECTRAS FOR THE CITY OF GUAYAQUIL, ECUADOR
ON THE CHAACTEISTICS OF SOFT SOIL INELASTIC DESIGN ESPONSE SPECTAS FO THE CITY OF GUAYAQUIL, ECUADO 837 Otton LAA 1 And moncao MACELO SUMMAY Five accelerograph records obtained in the cit of Guaaquil,
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 informationSimulation of Nonlinear Behavior of Wall-Frame Structure during Earthquakes
Simulation of Nonlinear Behavior of Wall-Frame Structure during Earthquakes b Masaomi Teshigawara 1, Hiroshi Fukuama 2, Hiroto Kato 2, Taiki Saito 2, Koichi Kusunoki 2, Tomohisa Mukai 2 ABSTRACT The reinforced
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 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 informationSimultaneous Orthogonal Rotations Angle
ELEKTROTEHNIŠKI VESTNIK 8(1-2): -11, 2011 ENGLISH EDITION Simultaneous Orthogonal Rotations Angle Sašo Tomažič 1, Sara Stančin 2 Facult of Electrical Engineering, Universit of Ljubljana 1 E-mail: saso.tomaic@fe.uni-lj.si
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 information8 Properties of Lamina
8 Properties of Lamina 8- ORTHOTROPIC LAMINA An orthotropic lamina is a sheet with unique and predictable properties and consists of an assemblage of fibers ling in the plane of the sheet and held in place
More informationAnalysis of Effects of Rebounds and Aerodynamics for Trajectory of Table Tennis Ball
SICE Annual Conference 21 August 18-21, 21, The Grand Hotel, Taipei, Taiwan Analsis of Effects of Reounds and Aerodnamics for Trajector of Tale Tennis Junko Nonomura Mechanical Science and Engineering,
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 informationBuckling Behavior of Long Symmetrically Laminated Plates Subjected to Shear and Linearly Varying Axial Edge Loads
NASA Technical Paper 3659 Buckling Behavior of Long Symmetrically Laminated Plates Sujected to Shear and Linearly Varying Axial Edge Loads Michael P. Nemeth Langley Research Center Hampton, Virginia National
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 informationMEG 741 Energy and Variational Methods in Mechanics I
MEG 74 Energ and Variational Methods in Mechanics I Brendan J. O Toole, Ph.D. Associate Professor of Mechanical Engineering Howard R. Hghes College of Engineering Universit of Nevada Las Vegas TBE B- (7)
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 informationJoule Heating Effects on MHD Natural Convection Flows in Presence of Pressure Stress Work and Viscous Dissipation from a Horizontal Circular Cylinder
Journal of Applied Fluid Mechanics, Vol. 7, No., pp. 7-3, 04. Available online at www.jafmonline.net, ISSN 735-357, EISSN 735-3645. Joule Heating Effects on MHD Natural Convection Flows in Presence of
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 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 informationUNCONVENTIONAL FINITE ELEMENT MODELS FOR NONLINEAR ANALYSIS OF BEAMS AND PLATES
UNCONVENTIONAL FINITE ELEMENT MODELS FOR NONLINEAR ANALYSIS OF BEAMS AND PLATES A Thesis by WOORAM KIM Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the
More informationFree Vibration Analysis of Kirchoff Plates with Damaged Boundaries by the Chebyshev Collocation Method. Eric A. Butcher and Ma en Sari
Free Vibration Analysis of Kirchoff Plates with Damaged Boundaries by the Chebyshev Collocation Method Eric A. Butcher and Ma en Sari Department of Mechanical and Aerospace Engineering, New Mexico State
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 informationTHE DIRIHLET PROBLEM FOR THE FRACTIONAL POISSON S EQUATION WITH CAPUTO DERIVATIVES A Finite Difference Approximation and a Numerical Solution
Beialaev, V. B., et al: The Dirihlet Prolem for the Fractional Poisson's Equation... THERMAL SIENE: Year, Vol. 6, No., pp. 385-394 385 THE DIRIHLET PROBLEM FOR THE FRATIONAL POISSON S EQUATION WITH APUTO
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 informationNatural frequencies of functionally graded plates by a meshless method
Composite Structures 75 (6) 53 6 www.elsevier.com/locate/compstruct Natural frequencies of functionall graded plates b a meshless method A.J.M. Ferreira a, *, R.C. Batra b, C.M.C. Roque a, L.F. Qian c,
More informationNumerical modelling of flexible pavement incorporating cross anisotropic material properties Part II: Surface rectangular loading
TCHNICAL PAPR Journal of the South African Institution of Civil ngineering ISSN 11-19 Vol 59 No 1, March 17, Pages 8 34, Paper 1385 PROF JAMS MAINA (Pr ng, MSAIC, FSAA) is a professional pavement engineer,
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 informationEVALUATION OF THERMAL TRANSPORT PROPERTIES USING A MICRO-CRACKING MODEL FOR WOVEN COMPOSITE LAMINATES
EVALUATION OF THERMAL TRANSPORT PROPERTIES USING A MICRO-CRACKING MODEL FOR WOVEN COMPOSITE LAMINATES C. Luo and P. E. DesJardin* Department of Mechanical and Aerospace Engineering Universit at Buffalo,
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 informationCHAPTER 5. Beam Theory
CHPTER 5. Beam Theory SangJoon Shin School of Mechanical and erospace Engineering Seoul National University ctive eroelasticity and Rotorcraft Lab. 5. The Euler-Bernoulli assumptions One of its dimensions
More informationAnalytical study of sandwich structures using Euler Bernoulli beam equation
Analtical stud of sandwich structures using Euler Bernoulli beam equation Hui Xue and H. Khawaja Citation: AIP Conference Proceedings 1798, 020076 (2017); doi: 10.1063/1.4972668 View online: http://dx.doi.org/10.1063/1.4972668
More informationHIGHER-ORDER THEORIES
HIGHER-ORDER THEORIES THIRD-ORDER SHEAR DEFORMATION PLATE THEORY LAYERWISE LAMINATE THEORY J.N. Reddy 1 Third-Order Shear Deformation Plate Theory Assumed Displacement Field µ u(x y z t) u 0 (x y t) +
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 informationVibration and Stability of a Composite Thin-Walled Spinning Tapered Shaft
Vibration and Stabilit of a Composite Thin-Walled Spinning Tapered Shaft Hungwon Yoon *, Sungsoo Na, Seok-Ju Cha * Korea Universit, Seoul, Korea, 3-7 Liviu Librescu Virginia Tech, Dept. of ESM, Blacksburg,
More informationThe Plane Stress Problem
. 14 The Plane Stress Problem 14 1 Chapter 14: THE PLANE STRESS PROBLEM 14 TABLE OF CONTENTS Page 14.1. Introduction 14 3 14.1.1. Plate in Plane Stress............... 14 3 14.1.. Mathematical Model..............
More informationConstants of Metal Rubber Material
Constants of Metal Rubber Material Modern Applied Science; Vol. 8, No. 5; 014 ISSN 1913-1844 E-ISSN 1913-185 Published b Canadian Center of Science and Education Aleander Mikhailovich Ulanov 1 1 Samara
More informationAPPLICATION OF DIRECT VARIATIONAL METHOD IN THE ANALYSIS OF ISOTROPIC THIN RECTANGULAR PLATES
VOL. 7, NO. 9, SEPTEMBER 0 ISSN 89-6608 006-0 Asian Research Publishing Network (ARPN). All rights reserved. APPLICATION OF DIRECT VARIATIONAL METHOD IN THE ANALYSIS OF ISOTROPIC THIN RECTANGULAR PLATES
More informationExercise solutions: concepts from chapter 5
1) Stud the oöids depicted in Figure 1a and 1b. a) Assume that the thin sections of Figure 1 lie in a principal plane of the deformation. Measure and record the lengths and orientations of the principal
More informationDr.Vinod Hosur, Professor, Civil Engg.Dept., Gogte Institute of Technology, Belgaum
STRUCTURAL DYNAMICS Dr.Vinod Hosur, Professor, Civil Engg.Dept., Gogte Institute of Technology, Belgaum Overview of Structural Dynamics Structure Members, joints, strength, stiffness, ductility Structure
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 informationMODELING OF NONLINEAR BEHAVIOR OF RC SHEAR WALLS UNDER COMBINED AXIAL, SHEAR AND FLEXURAL LOADING
CD02-003 MODELING OF NONLINEAR BEHAVIOR OF RC SHEAR WALLS UNDER COMBINED AXIAL, SHEAR AND FLEXURAL LOADING B. Ghiassi 1, M. Soltani 2, A. A. Tasnimi 3 1 M.Sc. Student, School of Engineering, Tarbiat Modares
More informationAnalytical Mechanics: Elastic Deformation
Analytical Mechanics: Elastic Deformation Shinichi Hirai Dept. Robotics, Ritsumeikan Univ. Shinichi Hirai (Dept. Robotics, Ritsumeikan Univ.) Analytical Mechanics: Elastic Deformation / 59 Agenda Agenda
More informationComposite Structures. Indian Institute of Technology Kanpur
Mechanics of Laminated Composite Structures Nachiketa Tiwari Indian Institute of Technology Kanpur Lecture 23 Analysis of an Orthotropic Ply Lecture Overview Introduction Engineering constants for an 2
More informationFig. 1. Circular fiber and interphase between the fiber and the matrix.
Finite element unit cell model based on ABAQUS for fiber reinforced composites Tian Tang Composites Manufacturing & Simulation Center, Purdue University West Lafayette, IN 47906 1. Problem Statement In
More informationEigenvalues of Trusses and Beams Using the Accurate Element Method
Eigenvalues of russes and Beams Using the Accurate Element Method Maty Blumenfeld Department of Strength of Materials Universitatea Politehnica Bucharest, Romania Paul Cizmas Department of Aerospace Engineering
More informationFlexural Analysis of Deep Aluminum Beam
Journal of Soft Computing in Civil Engineering -1 (018) 71-84 journal homepage: http://www.jsoftcivil.com/ Fleural Analysis of Deep Aluminum Beam P. Kapdis 1, U. Kalwane 1, U. Salunkhe 1 and A. Dahake
More informationIntroduction to structural dynamics
Introduction to structural dynamics p n m n u n p n-1 p 3... m n-1 m 3... u n-1 u 3 k 1 c 1 u 1 u 2 k 2 m p 1 1 c 2 m2 p 2 k n c n m n u n p n m 2 p 2 u 2 m 1 p 1 u 1 Static vs dynamic analysis Static
More information. D CR Nomenclature D 1
. D CR Nomenclature D 1 Appendix D: CR NOMENCLATURE D 2 The notation used by different investigators working in CR formulations has not coalesced, since the topic is in flux. This Appendix identifies the
More informationInternational Journal of Advanced Engineering Technology E-ISSN
Research Article INTEGRATED FORCE METHOD FOR FIBER REINFORCED COMPOSITE PLATE BENDING PROBLEMS Doiphode G. S., Patodi S. C.* Address for Correspondence Assistant Professor, Applied Mechanics Department,
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 informationHIGHER-ORDER THEORIES
HIGHER-ORDER THEORIES Third-order Shear Deformation Plate Theory Displacement and strain fields Equations of motion Navier s solution for bending Layerwise Laminate Theory Interlaminar stress and strain
More information