A parametric study on the elastic-plastic deformation of a centrally heated two-layered composite cylinder with free ends
|
|
- Morris Day
- 5 years ago
- Views:
Transcription
1 Arch. Mech., 68, 3, pp. 03 8, Warszawa 06 A parametric study on the elastic-plastic deformation of a centrally heated two-layered composite cylinder with free ends F. YALCIN ), A. OZTURK ), M. GULGEC 3) ) Hidromek,. Organize Sanayi Bölgesi Ankara, Turkey fatmayalcin003@gmail.com ) Department of Mechanical Engineering Necmettin Erbakan University Konya, Turkey aliozturk@konya.edu.tr 3) Department of Mechatronics Engineering Çankaya University Ankara, Turkey mgulgec@cankaya.edu.tr In this paper, an elastic-plastic deformation of a centrally heated two-layered composite cylinder with free ends subjected to uniformly distributed internal energy generation within an inner cylinder is studied using Tresca s yield condition and its associated flow rule. Stress, strain and displacement distributions in the composite cylinder made of elastic-perfectly plastic material are derived considering the influence of geometric parameters as well as material properties such as yield strength, modulus of elasticity, Poisson s ratio, coefficient of thermal conduction and coefficient of thermal expansion. Yielding starts at the outer boundary or at the axis corresponding to an edge regime of Tresca s prism in both cases. Propagations of the plastic regions are studied due to an increase of a heat generation. Key words: elastic-plastic stress analysis, thermal stress, composite cylinder, Tresca s criterion, yielding. Copyright c 06 by IPPT PAN. Introduction In many engineering applications, it is necessary to conduct an elasticplastic stress analysis. One of the reasons for this analysis is a thermal stress generated due to heat generation in bodies such as electrical conductors and nuclear reactors. The determination of the elastic-plastic and thermal stresses in cylindrical or spherical bodies has been achieved in a wide range of applications 4. Gulgec studied the influence of the temperature dependence of the
2 04 F. Yalcin, A. Ozturk, M. Gulgec yield stress on the stress distribution in a heat generating elastic-plastic cylinder with fixed ends 5. Different studies on the similar topic were also conducted by various authors 6 9. In a similar problem, Eraslan 0 subjected concentric tubes to free and radially constrained boundaries. In his study, the heat was assumed to be generated at a constant rate either within the inner or the outer tube. Orcan investigated the thermal stresses for both elastic and plastic deformations in a heat generating elastic-plastic homogeneous cylinder with free ends. More recently, Ozturk and Gulgec studied first an onset of yield due to material properties, and next they conducted an elastic-plastic stress analysis of two-layered heat generating composite cylinder with fixed ends, in addition to the effect of the material properties on the onset of yield due to thermal stresses, respectively, 3. The purpose of this paper is to obtain the complete solution and present a parametric analysis of elastic-plastic behaviour of the composite cylinder with free ends, which consists of two materials concentric to each other.. Problem statement and temperature distribution The geometry of the considered problem consists of an infinitely long solid cylinder of a radius a placed inside a tube with the inner radius a and the outer radius b Fig. ). This composite system is assumed to have free ends and the problem can be treated as a generalized plane strain problem. Since the end effects are ignored in the present analysis, the solution will be valid for sections located sufficiently away from the ends. It is assumed that heat is generated only within the inner cylinder at a uniform rate and transferred outside through the surrounding tube to an ambient kept at constant temperature. The material parameters are supposed to be independent of the temperature, because the equations derived in this paper are general equations that are not aimed for a specific material. It is not possible to derive a unique correlation for all materials, related with the dependence on the temperature. So, anyone who wants to use these equations for a specific material can insert the correlation for temperature dependence into the general equations and then follow the procedure given in this paper. The involved geometric and the thermo-mechanical parameters can be listed as follows: a,b: inner and outer radii of the tube, E,E : elasticity moduli, α,α : coefficients of thermal expansion, ν,ν : Poisson s ratios, λ,λ : σ I 0,σII 0 coefficients of thermal conduction, : yield strength of the solid cylinder and yield strength of the tube, respectively.
3 A parametric study on the elastic-plastic deformation Fig.. Composite cylinder geometry and plastic regions with their propagation directions e stands for elastic region, p for plastic region). The temperature distributions of the inner solid cylinder and the outer tube are denoted by T and T respectively. The reference temperature at the outer surface is T 0. The unsteady, coupled heat equation in polar coordinates, in its general form for the solid cylinder can be written as 4.) r r λ r T ) + ) T r r λ + ) T λ + q φ φ z z = ρ C p T t + 3λ + µ )α T D t, where r,φ,z are the cylindrical coordinates, t is the time, T is temperature distribution, q is internal energy generation per unit volume per unit time, ρ is the density, C p is the specific heat, λ and µ are Lame constants, and D is the dilatation. If the internal energy generation is slowly increased, the governing equation for the radial temperature distribution is reduced to:.) r r λ r T ) + q = 0. r The temperature distribution for the solid inner) cylinder becomes.3) T = q r 4λ + A lnr + A.
4 06 F. Yalcin, A. Ozturk, M. Gulgec At r = 0, T has to be finite, hence A = 0 and.4) T = q r 4λ + A. Solving Eq..) for q = 0, since there is no heat generation in the tube outer hollow cylinder), we find that.5) T = A 3 lnr + A 4. Using the conditions of continuity of the temperature and heat flux at the interface, the temperature is finite at r = 0 and equal to T 0 at r = b. The temperature distributions in the solid cylinder and in the tube take the following forms respectively: T = q r a + a ln a ).6) + T 0, 4 λ λ b T = q a.7) ln r λ b + T Elastic deformation By means of the basic equations of linear elasticity theory, the stress and the radial displacement distributions take the following forms Solid cylinder 3.) 3.) 3.3) 3.4) σ I r = E α ν ) θi 0,r) + C + C r, σ I θ = E α ν ) θi 0,r) T + C C r, σz I = E α ν ) T + ν C + E ε z, u I = + ν E C r + α + ν ν θ I 0,r) + C E + ν ) ν ) ν ε z r. 3.. Tube 3.5) 3.6) σ II r = E α ν ) θii a,r) + C 3 + C 4 r, σ II θ = E α ν ) θii a,r) T + C 3 C 4 r,
5 3.7) 3.8) A parametric study on the elastic-plastic deformation σ II z = E α ν ) T + ν C 3 + E ε z, u II = + ν C 4 E r + In the above expressions, θ I 0,r) = r α + ν ν θ II a,r) + C 3 E + ν ) ν ) ν ε z r 0 T r dr and θ II a,r) = r r a T r dr. The stresses and displacement are continuous at the interface and are bounded at the axis, the surface of the tube is free of any traction, and for an infinitely long cylinder with free ends a 0 b σzπrdr I + a σ II z πr dr = 0. When these conditions are enforced, it is found that C = 0 and the other unknowns are determined as follows: E α C = ν ) θi 0,a) + E α ν ) θii a,b) + C 4 a ) 3.9) b, E α C 3 = ν ) θii a,b) C 4 3.0) b, 3.) C 4 = θii a,b)d θ I 0,a) E α + E a b +ν ) E +ν ) ν ) where D = E σ0 II ν ) + E +ν ) ν ) α 3.) ε z = where E α ν ) a b λ q D = q a D 3 = θ II a,b) E σ II D 4 = +ν ) ν ) ν )), ν ) E ε z ν ν ) +ν ) ν ) ν ) + +ν, ) b a r. 4 a λ + λ ln a ) b + ν θ I 0,a) + E α ν ) D D 3 D 4 E E b ) + ν ν ) a +ν ) ν ) E, D 4 ln a b ) b + θ II a,b) ν + ν 0 ν ) + E + ν ) ν ) α +ν ) ν ) ν ) ) a b ν ν ) { a b + E E +ν ) +ν ) ν ) ν ) b + +ν ) a }. ) a, θ I E α 0,a) ν ),
6 08 F. Yalcin, A. Ozturk, M. Gulgec 3.3. Dimensionless parameters In order to generalize the obtained results, the parameters are made dimensionless as follows: r = r/b dimensionless radius, Q = a/b geometric parameter, E = E /E ratio of Young s moduli, ν = ν /ν ratio of Poisson s ratios, α = α /α ratio of thermal expansion coefficients, λ = λ /λ ratio of thermal conduction coefficients, σ 0 = σ0 II / σ I 0 ratio of yield limits, and q = q α E b ) / σ0 Iλ ) dimensionless thermal load parameter. The stress, displacement and plastic strain components are made dimensionless in the following forms: σ r = σ r σ I 0 ε p r = E ε p r σ I 0, σ θ = σ θ σ I 0, ε p θ = E ε p θ σ I 0, σ z = σ z σ0 I, u = E u σ0 Ib,, ε p z = E ε p z σ0 I, and the temperature distributions in the two layers are written in dimensionless forms as T = T T 0 )E α / σ I 0 and T = T T 0 )E α / σ I 0 Fig. ). Fig.. Dimensionless nondimensional) temperature distribution for Q = 0.5, q = 5, λ = 0.3, λ =.0 and λ = Elastic limit analysis The elastic-plastic constitutive equations for the generalized plane strain problem in cylindrical coordinates are given by 5:
7 A parametric study on the elastic-plastic deformation ) 3.4) 3.5) ε r = E σ r νσ θ + σ z ) + α T + ε p r, ε θ = E σ θ νσ r + σ z ) + α T + ε p θ, ε z = E σ z νσ r + σ θ ) + α T ε p r + ε p θ ), where ε z = constant for generalized plane strain. Assuming that the two layers forming the composite tube have the same thermo-mechanical properties E =, α =, λ =, ν =, σ 0 =, the dependence of onset of yield at the axis and at the surface on the geometric parameter Q = a/b is investigated. Yielding starts both at the surface and at the axis of the composite cylinder for Q Fig. 3). It is noted that the thermal load required for the onset of yield increases exponentially as the geometric parameter Q decreases. Fig. 3. Dependence of onset of yield on the geometric parameter Q for Ē =, ᾱ =, λ =, ν = and σ 0 =. 4. Onset of yield at the surface of the composite cylinder Yielding starts at the surface of the composite cylinder in which the stress state corresponds to an edge regime of Tresca s yield surface with the principal stresses σ θ = σ z > σ r. Two plastic regions develop simultaneously and expand inwards through the tube, while the solid cylinder stays purely elastic Fig. ). In this section, the general equations for determining the plastic stress-strain relations for Tresca s yield criterion are derived based on a unified approach by Drucker 5.
8 0 F. Yalcin, A. Ozturk, M. Gulgec 4.. Plastic region r 4 < r < b) 4.) 4.) In this edge regime, Tresca s yield functions and the associated flow rule 6 f = σ θ ) II σ r ) II σ II 0, f = σ z ) II σ r ) II σ II 0 4.3) dε p ij = k f k σ ij dλ k lead to 4.4) dε p ij = k= f k σ ij dλ k = f σ ij dλ + f σ ij dλ which, when substituting non-zero stress components, results in 4.5) 4.6) 4.7) dε p θ = dε p z = dε p r = k= k= k= f k σ θ dλ k = f σ θ dλ + f σ θ dλ = dλ, f k σ z dλ k = f σ z dλ + f σ z dλ = dλ, f k σ r dλ k = f σ r dλ + f σ r dλ = dλ + dλ ). Applying these relations to the plastic region, we obtain: dε p θ )II = dλ, dε p z) II = dλ and dε p r) II = dλ + dλ ), where the subscripts and of dλ are only index numbers, irrelevant to the plastic region numbers. Hence, 4.8) dε p r) II = dε p θ )II + dε p z) II, where the superscript II denotes the tube, and the subscript the plastic region. According to Eqs. 4.) and 4.), the equation of equilibrium leads to 4.9) 4.0) σ r ) II = σ II 0 lnr + C 5, σ z ) II = σ θ ) II = σ II 0 + ln r) + C 5. Using plastic incompressibility, the elastic formula for dilatation leads to a differential equation for the radial displacement with the general solution 4.) u II = ν ) r σ0 II E + 3ln r + 3C 5 + 3α rθ II r 4,r) ε zr + C 6 r,
9 where A parametric study on the elastic-plastic deformation... r θ II r 4,r) = r T r)rdr. r 4 The plastic strains are then obtained as 4.) 4.3) ε p r) II = ν E σii 0 ln r + C ν 4E σ II 0 α 3θ II r 4,r) T r) ε z C 6 r, ε p z) II = ε z E ν )σ II 0 + ν )σ II 0 lnr + C 5 ) α T r). 4.. Plastic region r 3 < r < r 4 ) In this plastic region, due to the inequality σ θ ) II > σ z ) II > σ r ) II, we obtain 4.4) f = σ θ ) II σ r ) II σ II 0, and thus the following can be written: dε p r) II = dε p θ )II, dεp z) II = 0. The stresses, displacement and plastic strains are derived as 4.5) 4.6) 4.7) 4.8) 4.9) where σ r ) II = σ II 0 ln r + C 7, σ θ ) II = σ II 0 + ln r) + C 7, u II ε p θ )II = + ν ) ν ) E rσ II 0 ln r + C ν )α rθ II r 3,r) ν ε z r + C 8 r, = ν) σii ν )α θ II r 3,r) T r) + C 8 E r, ε p r) II = ε p θ )II, r θ II r 3,r) = r T r)rdr. r Conditions and determination of the unknowns Two elastic regions surrounded by two plastic regions contain unknowns: C, C, C 3, C 4, C 5, C 6, C 7, C 8, the axial strain ε z, and the border radii r 3 and r 4.
10 F. Yalcin, A. Ozturk, M. Gulgec For the determination of these unknowns, the following boundary and continuity conditions are enforced: 4.0) 4.) 4.) 4.3) 4.4) 4.5) 4.6) 4.7) 4.8) 4.9) 4.30) a 0 σ z ) I er dr + at r = 0 at r = a at r = a at r = r 3 at r = r 3 at r = r 3 at r = r 4 at r = r 4 at r = r 4 at r = b r3 a u I e is finite, σ r ) II e = σ r ) I e, u) II e = u) I e, σ r ) II e = σ r ) II, ε p θ )II = 0, σ θ ) II e σ r ) II e = σ II 0, σ r ) II = σ r ) II, σ θ ) II = σ z ) II, ε p θ )II = ε p θ )I, σ r ) II = 0, σ z ) II e r dr + r4 r3 b σ z ) II r dr + r4 σ z ) II r dr = 0, where the last one is the free end condition. They result in C = 0 and 4.3) 4.3) 4.33) 4.34) 4.35) 4.36) 4.37) E α C = ν ) θi 0,a) + C 3 E α C 3 = C 4 = r 3 C 5 = σ0 II lnb, C 7 = C 5, + C 4 a ν ) θii a,r 3 ) + σ II 0 ln r 3, b C 4 r 3 E α ν ) θii a,r 3 ) T r 3 ) σ0 II E ε z = σ0 II ν + ν ) ln r 4 b C 6 = C 8 σii 0 + r4 ν 4ν E,, + E α T r 4 ), + ν ) ln r 4 b 4.38) α r4ν T r 4 ) + ν )θ II r 3,r 4 ) + ε zr4, C 8 = r3 ν ) σii ν )α T r 3 ), E
11 4.39) A parametric study on the elastic-plastic deformation ν ) ν ) C E ν ν )ε z = + ν ) ν ) C 3 E α + ν ν θ I 0,a) + ν E C 4 a. The integrals in Eq. 4.30) are evaluated as a σ z ) I er dr = E α a 4 +a 4 + λ ln a ) 4.40) 6 ν ) λ b 4.4) 4.4) 4.43) r3 a r4 r3 b r4 + ν C +ε z E )a, σ z ) II e r dr = E α q λ 4 ν ) a r3 ln r 3 ) a b ln a ) b + ν C 3 +E ε z )r 3 a ), σ z ) II E α q r dr = λ 4 a +ν σ0 II r4 ln r ) 4 b r3 ln r ) 3 b + r 4 r 3 b σ z ) II r dr = 4 r 4 ν σ II 0 +E ε z ), ln r ) 4 b +. The border radii r 3 and r 4 are evaluated from the simultaneous solutions of the free surface condition and Eq. 4.30). 5. Onset of yield at the axis of the solid cylinder For smaller values of the geometric parameter Q = a/b yielding starts first at the center of the composite cylinder and the two plastic regions, plastic regions 3 and 4 expand outward simultaneously with different rates of propagation Fig. ). Stress states in the principal stress space corresponds to σ θ = σ r > σ z and σ θ > σ r > σ z respectively. 5.. Plastic region 3 0 < r < r ) In this edge regime, the two yield functions 5.) 5.) f = σ θ ) I 3 σ z ) I 3 σ I 0, f = σ r ) I 3 σ z ) I 3 σ I 0
12 4 F. Yalcin, A. Ozturk, M. Gulgec lead to 5.3) 5.4) σ r ) I 3 = σ θ ) I 3 = C 9, σ z ) I 3 = C 9 σ I 0. Using plastic incompressibility, we obtain the differential equation 5.5) du I 3 dr + ui 3 r = ν ) σ r ) I 3 + σ θ ) I 3 + σ z ) I 3 + 3α T r) ε z with the general solution 5.6) u I 3 = ν E E The plastic strains are then as follows: 5.7) 5.8) 5.9) r 3C 9 σ I 0 + 3α rθ I 0,r) ε zr + C 0 r. ε p θ )I 3 = E ν )C 9 σ I 0 + α 3θ I 0,r) T r) ε z + C 0 r, ε p r) I 3 = E ν )C 9 σ I 0 α 3θ I 0,r) T r) ε z C 0 r, ε p z) I 3 = ε z E ν )C 9 σ I 0 α T r). 5.. Plastic region 4 r < r < r ) By using the yield function 5.0) f = σ θ ) I 4 σ z ) I 4 σ I 0, the plastic strain increments dε p z) I 4 = dεp θ )I 4, dεp r) I 4 = 0, the equilibrium and the compatibility equations, we derive the following differential equation for the tangential stress: 5.) r d σ θ ) I 4 dr + 3r dσ θ) I 4 + ν ) dr = with the general solution ν ) ν ) σ θ) I 4 σ I0 E α T + 5r dt dr + T rd dr ) + E ε z, 5.) σ θ ) I 4 = C r M) + C r +M) + σi 0 + E ε z ) v + E α 4 v ) + M)θ + + M)θ 4T,
13 5.3) where A parametric study on the elastic-plastic deformation... 5 σ r ) I 4 = { C r M) C r +M) M + E } α 4 v ) M)θ + M)θ + v ) σi 0 + E ε z ), r θ = r M) r T r M dr, r θ = r +M) T r M dr, r M = ν ). Therefrom, the radial displacement and the plastic strain components are defined as { E u I 4 = v v ) C r M + M 5.4) M 4 v ) E α θ r + v + v ) C r M + + M } M 4 v ) E α θ r 5.5) + + v )σ0r I + E ε z r, E ε p θ )I 4 = v v ) C r M) + M + v + v M 5.3. Conditions and determination of the unknowns M) 4 v ) E α θ ) C r +M) + + M 4 v ) E α θ For the determination of the unknowns: C, C, C 3, C 4, C 9, C 0, C, C the axial strain ε z, and the border radii r and r, the following boundary and continuity conditions are used: 5.6) at r = 0 u I 3 is finite, 5.7) at r = r σ r ) I 3 = σ r) I 4, 5.8) at r = r σ θ ) I 3 = σ θ) I 4, 5.9) at r = r ε p r) I 3 = 0,.
14 6 F. Yalcin, A. Ozturk, M. Gulgec 5.0) at r = r ε p θ )I 4 = 0, 5.) at r = r σ r ) I 4 = σ r) I e, 5.) at r = r σ θ ) I e = σ θ ) I 4, 5.3) at r = a σ r ) II e = σ r ) I e, 5.4) at r = a u) II e = u) I e, 5.5) at r = b σ r ) II e = 0, 5.6) r 0 σ z ) I 3 r dr + r r a σ z ) I 4 r dr + The above conditions lead to C 0 = 0 and C = + ) C r M) + ) 5.7) M M + ) M)θ r,r )+ M r b σ z ) I e r dr + a σ z ) II e r dr = 0. C r +M) + E α 4 ν ) M ) +M)θ r,r ) 5.8) 5.9) 5.30) 5.3) 5.3) 5.33) + ν ) σi 0+E ε z ), C = ) C r +M + M M E α C 3 = C 4 = a b b a ) + M ) M)θ r,r )+ ν ) θii a,b) C 4 b, ) C r M + M E α 8 ν ) ) +M)θ r,r ) E α ν ) θi r,a) E α ν ) θii a,b)+ C + C a C 9 = ν ) E α 3θ I 0,r ) T r )+E ε z +σ0, I C = { E α r M) 6+M) ν ) θi 0,r ) + ν ) 4+M) ν ) C = { E α r +M) 6 M) ν ) θi 0,r ) + ν ) 4 M) ν ), r, } T r ), } T r ),
15 A parametric study on the elastic-plastic deformation ) ε z = { C a +ν ) E b b a +ν ) E +ν ) ν ) E a } b +θ I r,a) { α +ν ) ν + a b E α b a ) ν ) +ν ) E +ν ) ν )} a E b { ) + M C r M) + ) M C r +M) + ν ) σi 0 + E α ) 4 ν ) + M θ r,r ) M)+ ) M +M)θ r,r ) } { E +ν ) ν ) a b b a ) +ν ) E +ν ) ν )} a E b +ν ν )ε z + E α ν ) θii a,b) { a b b a ) +ν ) E +ν ) ν ) a E b +ν ) ν )} E +ν )+ ν ) { E+ν. )+Q ν )}+ν ν ) +Q ) From Eq. 5.0) we have the following relationship: 5.35) ν ν M + ν + ν M ) C r M) + M) 4 ν ) E α θ r,r ) ) C r +M) + M) + 4 ν ) E α θ r,r ) and the integrals in the free end condition take the following forms: = 0, 5.36) 5.37) 5.38) r 0 r r r σ z ) I 3r dr = C 9 σ I 0) r, σ z ) I 4r dr = C r +M r +M ) + M + C r M r M ) M + E 4 V ) M) + E ε z + ν σ0 I V ) r r θ r,r)r dr r + + M) θ r,r)r dr 4 r r θ r,r)r dr = q 4 r r T r)r dr r r ), r 4 r4 4λ 3 M) + a + ln a ) M λ λ b
16 8 F. Yalcin, A. Ozturk, M. Gulgec { r r ) M) } r r r + M r ) M) r r r r + M) r λ 3 M) r q r 4 θ r,r)r dr = r4 5.39) 4 4λ 3 + M) + a + M r { r r ) +M) } r r r M r ) +M) r r r r M) r λ 3 M) r q r 4 T r)r dr = r ) 4 r a 5.4) σ z ) I er dr r = E α q a 4 r 4 ν ) 4 5.4) b a + ν C + E ε z ) a r ),, λ + λ ln a b, + r r ) { a + ln a 4λ λ λ b + a r ) a + ln a 4λ λ λ b σ z ) II er dr = ν C 3 + E ε z )b a ) + E α q a ν ) λ b ln b b ) a ln a b ). In the first stage of elastic-plastic deformation, the border radii r and r are evaluated as a function of the thermal load from the simultaneous solution of Eqs. 5.6) and 5.35). 6. Onset of yield at the interface of the composite cylinder Depending on the choice of the material parameters, beyond a certain critical load parameter, another plastic region, plastic region 5 can be generated at the outer surface of solid cylinder the interface of the composite cylinder). This region propagates inwards as plastic regions 3 and 4 expand outwards until they meet when the elastic region vanishes and the solid cylinder reaches the fully plastic state Fig. ). ) ) },
17 A parametric study on the elastic-plastic deformation Plastic region 5 r 5 < r < a) In this region,σ θ ) I 5 > σ z) I 5 > σ r) I 5 and the yield function 6.) f = σ θ ) I 5 σ r ) I 5 σ I 0 requires that dε p r) I 5 = dεp θ )I 5 and dεp z) I 5 = 0. Hence, 6.) 6.3) 6.4) 6.5) 6.6) where σ r ) I 5 = σ I 0 ln r + C 3, σ θ ) I 5 = σ I 0 + lnr) + C 3, σ z ) I 5 = ν σ I 0ln r + ) + C 3 + E ε z E α T r), u I 5 = + ν ) ν ) E rσ I 0 lnr + C 3 ) + + ν )α rθ I r 5,r) ν ε z r + C 4 r, ε p θ )I 5 = ν ) σi 0 E + + ν )α θ II r 5,r) T r) + C 4 r, r θ I r 5,r) = r T r)r dr. r Conditions and results For this stage of plastic deformation, the total number of unknowns is 7 and they are C, C, C 5, C 6, C 7, C 8, C 9, C 0, C, C, C 3, C 4, ε z, r, r, r 4 and r 5. In Section 5.3, the unknowns C, C, C 9, C 0, C, C were determined, and in Section 4.3, the unknowns C 5, C 6, C 7, ε z were defined. Using the conditions: ε p θ )I 5 = 0 at r = r 5, σ r ) II = σ r) I 5 that 6.7) 6.8) 6.9) { C 8 = a σ0 II ln a + ν ) ν ) b and u)ii = u)i 5 at r = a = r 3, it follows + ν ) ν ) E E + + ν )α θ I r 5,a) + ν ν )ε Z + C 4 a C 3 = σ0 II ln a b σi 0 ln a, { } C 4 = r5 ν) σi ν )α T I r 5 ). E The unknown border radii will be determined from the simultaneous solution of the following nonlinear equations: },
18 0 F. Yalcin, A. Ozturk, M. Gulgec 6.0) 6.) 6.) ν ν M + ν + ν M ) C r M) + M) 4 ν ) E α θ r,r ) ) C r +M) + M) + 4 ν ) E α θ r,r ) σ0 I lnr 5 + C 3 + E α ν ) θi r,r 5 ) C C r5 = 0, ν ) E α θ I r,r 5 ) E α ν ) T r 5 ) C r5 σ0 II = 0, and the free end condition is = 0, 6.3) r 0 σ z ) I 3r dr + r r σ z ) I 4r dr + a + r5 r5 r σ z ) I 5r dr + σ z ) I er dr r4 a b σ z ) II r dr + r4 σ z ) II r dr = 0, where 6.4) a r 5 σ z ) I 5r dr = ν σ I 0 + E α q 4 a r { a 4 r5 4 + a r5 4λ 5) σii 0 σ0 I ln a b r 5 ln r 5 a a λ + λ ln a b )} a r5 + E ε z. 7. Numerical results In this section, the conditions for the onset of yield and the effects of all the parameter ratios on the distribution of stresses and plastic strains in different stages of elastic-plastic deformations are investigated. In the presentation of the numerical results, the ratios of the material parameters are taken as.0 unless they are specified differently. 7.. Effect of the parameter Q First, the case in which all the dimensionless parameters are taken as.0 is considered. Yielding starts simultaneously both at the axis and at the surface of the composite cylinder for the dimensionless load parameter q =7.54 and for the geometric parameter Q= For the values less than the critical value of 0.499, yielding starts at the axis and for the values greater than the critical
19 A parametric study on the elastic-plastic deformation... value of yielding starts at the outer surface. For Q=0.4 < as shown in Fig. 4, yielding starts first at the axis at q =8.43 for σ 0 =, and plastic regions 3 and 4 expand outward with increasing thermal loads. At q =9.56 the elastic-plastic behavior of the composite cylinder enters the second stage in which plastic flow starts at the outer surface, and plastic regions and propagate inward. The plastic-elastic border r reaches the interface at r = a and q =3.59, while the inner portion of the outer cylinder is still elastic. The stresses and deformations corresponding to q =0.944 are plotted in Fig. 5. The composite cylinder reaches the fully plastic state with r = a = r 3 at q = Fig. 4. Expansion of plastic regions as a function of the load parameter for Q = 0.4, σ 0 =.0 and σ 0 = Effect of the parameter σ 0 It was shown in Fig. 4 that for σ 0 = yielding starts at the axis when Q = 0.4. On the other hand, for small values of the yield limit ratios yielding starts first at the outer surface of the tube. For σ 0 = 0.6, the corresponding load parameter of the onset of yield at the surface of the tube is q =.5. In Fig. 5, the stresses and the deformations are compared for the chosen yield limit ratios. If the yield limit ratio is decreased further, yielding starts again at the
20 F. Yalcin, A. Ozturk, M. Gulgec Fig. 5. a) Stresses and displacement, b) plastic strains for Q = 0.4, q = 0.944, σ 0 =.0 and σ 0 = 0.6. outer surface, but this time at smaller load parameters. When Q = 0.8 for both σ 0 =.0 and σ 0 =.4 yielding starts at the surface for the load parameters of q = and q = respectively, while the tube has a relatively higher resistance to yielding.
21 A parametric study on the elastic-plastic deformation... 3 Fig. 6. a) Stresses and displacement; b) plastic strains for Q = 0.6, q = 5, E =.0 and E =.5.
22 4 F. Yalcin, A. Ozturk, M. Gulgec 7.3. Effect of the parameter E The effect of the parameter E on the stress and deformation distribution in the second stage of elastic-plastic behavior is shown in Fig. 6. For Q = 0.6 and q = 5 for E =, the border radii are evaluated as r = 0.546, r = , r 3 = 0.668, r 4 = ; whereas for E =.5 the border radii are evaluated as r = , r = 0.46, r 3 = and r 4 = It is shown that, as the Young modulus of the inner component becomes greater, i.e., for E >, the inner and outer plastic regions stay in a narrow range. However, the inner and outer plastic regions propagate faster for E <. For the same geometric parameters Q = 0.5, q = 5 and E = 0.5, the border radii become r = , r = 0.33, r 3 = and r 4 = , which justifies the case presented above Effect of the parameter ν For Q = 0.6, q = 5 and ν =, the radii were given in the previous section. For ν = 0.7, we have r = , r = , r 3 = and r 4 = This shows that as ν gets smaller all of the plastic regions cannot expand at the same rate. For Q = 0.5, q = 5 and ν =, the border radii are r = 0.098, r = , r 3 = , r 4 = , whereas for ν =.38, the border radii become r = , r = , r 3 = 0.585, r 4 = Compared with ν =, it is found that when ν > the plastic regions expand at a faster rate. In Fig. 7, it can be also noted that the plastic strains for ν > are considerably greater than those for ν = at the same load parameter Effect of the parameter λ The effect of the parameter λ on the temperature distribution was shown in Fig.. As λ increases the temperature distribution inside the composite cylinder increases. The effect of λ on elastic-plastic stress distribution is evident from its contribution on the temperature distribution. For Q = 0.6, q = 5 and λ = 0.6 the border radii are r = 0.03, r = , r 3 = and r 4 = 0.957; whereas for λ = they become r = 0.546, r = , r 3 = and r 4 = Effect of the parameter α The effect of the coefficient of thermal expansion ratio α is shown in Fig. 8. For Q = 0.5 and q = 5 when α =., the border radii easily propagate except for the outermost plastic region) and become r = , r = 0.505, r 3 = and r 4 = On the other hand, for α = 0.8 the border radii
23 A parametric study on the elastic-plastic deformation... 5 Fig. 7. a) Stresses and displacement, b) plastic strains for Q = 0.5, q = 5, ν =.0 and ν =.38.
24 6 F. Yalcin, A. Ozturk, M. Gulgec Fig. 8. a) Stresses and displacement, b) plastic strains for Q = 0.5, q = 5, ᾱ =.0 and ᾱ =..
25 A parametric study on the elastic-plastic deformation... 7 are r = , r = 0.668, r 3 = and r 4 = , which shows that the expansion of plastic regions is retarded for α <. 8. Conclusions The advantage of using a two-layered composite cylinder, due to its higher thermal load carrying capacity, becomes apparent when the results presented in this study are compared to those given by ORCAN for a homogeneous solid cylinder in. As the thickness of the tubular shell is increased, onset of yield at the outer surface and its propagation become more difficult, and for sufficiently small values of the geometric parameter Q, yielding occurs at the axis if higher thermal load is supplied. The choice of the greater Young modulus for the solid cylinder, i.e., as E increases, causes the propagation of plastic regions to become more difficult, leading to wider elastic regions. On the other hand, choosing smaller values for each of the parameters ν, α and λ results in a retardation of the expansion of plastic regions. It is concluded that thermally induced elasticplastic deformations of the composite cylinder can be decreased significantly by a proper selection of the ratios of thermo-mechanical properties. References. Z. Mróz, K. Kowalczyk Gajewska, J. Maciejewski, R.B. Pęcherski, Tensile or compressive plastic deformation of cylinders assisted by cyclic torsion, Arch. Mech., 58, 6, , I.-D. Ghiba, On the deformation of transversely isotropic porous elastic, circular cylinder, Arch. Mech., 6, 5, 407 4, L. H. You, Z. Y. Zheng, Elastic plastic thermo-mechanical response of composite coaxial cylinders, J. Mater. Sci., 4, 5, , Y. Orcan, U. Gamer, Elastic-plastic deformation of a centrally heated cylinder, Acta Mech., 90, 4, 6 80, M. Gulgec, Influence of the temperature dependence of the yield stress on the stress distribution in a heat generating elastic-plastic cylinder, ZAMM, 79, 3, 0 6, M. Gulgec, Y. Orcan, Elastic-plastic deformation of a heat generating tube with temperature dependent yield stress, Int. J. Eng. Sci., 38,, 89 06, Y. Orcan, M. Gulgec, Influence of the temperature dependence of the yield stress on the stress distribution in a heat-generating tube with free ends, J. Therm. Stress., 3, 6, , C.L. Tan, K.H. Lee, Elastic-plastic stress analysis of a cracked thick-walled cylinder, J. Strain Analysis, 8, 4, 53 60, M.A. Irfan, W. Chapman, Thermal stresses in radiant tubes due to axial, circumferential and radial temperature distributions, Appl. Therm. Eng., 9, 0, 93 90, 009.
26 8 F. Yalcin, A. Ozturk, M. Gulgec 0. A.N. Eraslan, Stress distribution in energy generating two-layer tubes subjected to free and radially constrained boundary conditions, Int. J. Mech. Sci., 45, 3, , Y. Orcan, Thermal stresses in a heat generating elastic-plastic cylinder with free ends, Int. J. Eng. Sci., 3, 8, , A. Ozturk, M. Gulgec, Determination of onset of yield due to material properties in a heat generating two-layered compound cylinder, Applied Mechanics and Materials, 35-36, 7, A. Ozturk, M. Gulgec, Influence of the material properties on the elastic-plastic deformation in a heat generating composite solid cylinder, Journal of the Faculty of Engineering and Architecture of Gazi University, 8,, 83 9, F.P. Incropera, D.P. De Witt, Fundamentals of Heat and Mass Transfer, p. 45, nd Ed., John Wiley & Sons, New York, A. Mendelson, Plasticity: Theory and Application, p. 37, pp. 6, Macmillan, New York, W.T. Koiter, General theorems for elastic-plastic solids, in: Progress in Solid Mechanics, I.N. Sneddon and R. Hill Eds., North-Holland Publishing Company, Amsterdam, pp. 65, 960. Received November 4, 05; revised version April 3, 06.
The 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 informationPractice Final Examination. Please initial the statement below to show that you have read it
EN175: Advanced Mechanics of Solids Practice Final Examination School of Engineering Brown University NAME: General Instructions No collaboration of any kind is permitted on this examination. You may use
More informationLecture 8. Stress Strain in Multi-dimension
Lecture 8. Stress Strain in Multi-dimension Module. General Field Equations General Field Equations [] Equilibrium Equations in Elastic bodies xx x y z yx zx f x 0, etc [2] Kinematics xx u x x,etc. [3]
More informationStress analysis of functionally graded discs under mechanical and thermal loads
Indian Journal of Engineering & Materials Sciences Vol. 8, April 0, pp. -8 Stress analysis of functionally graded discs under mechanical and thermal loads Hasan Çallioğlu, Metin Sayer* & Ersin Demir Department
More informationAdvanced Structural Analysis EGF Cylinders Under Pressure
Advanced Structural Analysis EGF316 4. Cylinders Under Pressure 4.1 Introduction When a cylinder is subjected to pressure, three mutually perpendicular principal stresses will be set up within the walls
More informationReference material Reference books: Y.C. Fung, "Foundations of Solid Mechanics", Prentice Hall R. Hill, "The mathematical theory of plasticity",
Reference material Reference books: Y.C. Fung, "Foundations of Solid Mechanics", Prentice Hall R. Hill, "The mathematical theory of plasticity", Oxford University Press, Oxford. J. Lubliner, "Plasticity
More informationThermoelastic Stresses in a Rod Subjected to Periodic Boundary Condition: An Analytical Treatment
Thermoelastic Stresses in a Rod Subjected to Periodic Boundary Condition: An Analytical Treatment Ahmet N. Eraslan Department of Engineering Sciences Middle East Technical University Ankara 06531, Turkey
More informationARTICLE A-8000 STRESSES IN PERFORATED FLAT PLATES
ARTICLE A-8000 STRESSES IN PERFORATED FLAT PLATES Delete endnote 18, which says "Express metric values in exponential form" A-8100 INTRODUCTION A-8110 SCOPE (a) This Article contains a method of analysis
More informationModule 7: Micromechanics Lecture 29: Background of Concentric Cylinder Assemblage Model. Introduction. The Lecture Contains
Introduction In this lecture we are going to introduce a new micromechanics model to determine the fibrous composite effective properties in terms of properties of its individual phases. In this model
More informationROTATING RING. Volume of small element = Rdθbt if weight density of ring = ρ weight of small element = ρrbtdθ. Figure 1 Rotating ring
ROTATIONAL STRESSES INTRODUCTION High centrifugal forces are developed in machine components rotating at a high angular speed of the order of 100 to 500 revolutions per second (rps). High centrifugal force
More informationMechanical Engineering Ph.D. Preliminary Qualifying Examination Solid Mechanics February 25, 2002
student personal identification (ID) number on each sheet. Do not write your name on any sheet. #1. A homogeneous, isotropic, linear elastic bar has rectangular cross sectional area A, modulus of elasticity
More informationA simple plane-strain solution for functionally graded multilayered isotropic cylinders
Structural Engineering and Mechanics, Vol. 24, o. 6 (2006) 000-000 1 A simple plane-strain solution for functionally graded multilayered isotropic cylinders E. Pan Department of Civil Engineering, The
More informationChapter 3. Load and Stress Analysis
Chapter 3 Load and Stress Analysis 2 Shear Force and Bending Moments in Beams Internal shear force V & bending moment M must ensure equilibrium Fig. 3 2 Sign Conventions for Bending and Shear Fig. 3 3
More informationAnalytical and Numerical Solutions to a Rotating FGM Disk
one parametric exponential model Journal of Multidisciplinary Engineering Science Technology (JMEST) Analytical Numerical Solutions to a Rotating FGM Disk Ahmet N. Eraslan Department of Engineering Sciences
More informationA study of forming pressure in the tube-hydroforming process
Journal of Materials Processing Technology 192 19 (2007) 404 409 A study of forming pressure in the tube-hydroforming process Fuh-Kuo Chen, Shao-Jun Wang, Ray-Hau Lin Department of Mechanical Engineering,
More informationRadial Growth of a Micro-Void in a Class of. Compressible Hyperelastic Cylinder. Under an Axial Pre-Strain *
dv. Theor. ppl. Mech., Vol. 5, 2012, no. 6, 257-262 Radial Growth of a Micro-Void in a Class of Compressible Hyperelastic Cylinder Under an xial Pre-Strain * Yuxia Song, Datian Niu and Xuegang Yuan College
More informationPrediction of Elastic Constants on 3D Four-directional Braided
Prediction of Elastic Constants on 3D Four-directional Braided Composites Prediction of Elastic Constants on 3D Four-directional Braided Composites Liang Dao Zhou 1,2,* and Zhuo Zhuang 1 1 School of Aerospace,
More informationAn alternative design method for the double-layer combined die using autofrettage theory
https://doi.org/10.5194/ms-8-267-2017 Author(s) 2017. This work is distributed under the Creative Commons Attribution.0 License. An alternative design method for the double-layer combined die using autofrettage
More informationMicrostructural effect on the cavity expansion in a soil cylinder
Microstructural effect on the cavity expansion in a soil cylinder J.D. Zhao, D.C. Sheng & S.W. Sloan Centre for Geotechnical and Materials Modelling, School of Engineering University of Newcastle, Callaghan,
More informationA note on finite elastic deformations of fibre-reinforced non-linearly elastic tubes
Arch. Mech., 67, 1, pp. 95 109, Warszawa 2015 Brief Note A note on finite elastic deformations of fibre-reinforced non-linearly elastic tubes M. EL HAMDAOUI, J. MERODIO Department of Continuum Mechanics
More informationLecture #6: 3D Rate-independent Plasticity (cont.) Pressure-dependent plasticity
Lecture #6: 3D Rate-independent Plasticity (cont.) Pressure-dependent plasticity by Borja Erice and Dirk Mohr ETH Zurich, Department of Mechanical and Process Engineering, Chair of Computational Modeling
More informationStresses Analysis of Petroleum Pipe Finite Element under Internal Pressure
ISSN : 48-96, Vol. 6, Issue 8, ( Part -4 August 06, pp.3-38 RESEARCH ARTICLE Stresses Analysis of Petroleum Pipe Finite Element under Internal Pressure Dr.Ragbe.M.Abdusslam Eng. Khaled.S.Bagar ABSTRACT
More informationAnalysis of asymmetric radial deformation in pipe with local wall thinning under internal pressure using strain energy method
Analysis of asymmetric radial deformation in pipe with local wall thinning under internal pressure using strain energy method V.M.F. Nascimento Departameto de ngenharia Mecânica TM, UFF, Rio de Janeiro
More informationDistributed: Wednesday, March 17, 2004
MASSACHUSETTS INSTITUTE OF TECHNOLOGY DEPARTMENT OF MECHANICAL ENGINEERING CAMBRIDGE, MASSACHUSETTS 019.00 MECHANICS AND MATERIALS II QUIZ I SOLUTIONS Distributed: Wednesday, March 17, 004 This quiz consists
More informationLinearized theory of elasticity
Linearized theory of elasticity Arie Verhoeven averhoev@win.tue.nl CASA Seminar, May 24, 2006 Seminar: Continuum mechanics 1 Stress and stress principles Bart Nowak March 8 2 Strain and deformation Mark
More informationE. not enough information given to decide
Q22.1 A spherical Gaussian surface (#1) encloses and is centered on a point charge +q. A second spherical Gaussian surface (#2) of the same size also encloses the charge but is not centered on it. Compared
More informationFigure 2-1: Stresses under axisymmetric circular loading
. Stresses in Pavements.1. Stresses in Fleible Pavements.1.1. Stresses in Homogeneous Mass Boussinesq formulated models for the stresses inside an elastic half-space due to a concentrated load applied
More informationTHERMOELASTIC ANALYSIS OF THICK-WALLED FINITE-LENGTH CYLINDERS OF FUNCTIONALLY GRADED MATERIALS
Journal of Thermal Stresses, 28: 391 408, 2005 Copyright # Taylor & Francis Inc. ISSN: 0149-5739 print/1521-074x online DOI: 10.1080/01495730590916623 THERMOELASTIC ANALYSIS OF THICK-WALLED FINITE-LENGTH
More informationAnalytical formulation of Modified Upper Bound theorem
CHAPTER 3 Analytical formulation of Modified Upper Bound theorem 3.1 Introduction In the mathematical theory of elasticity, the principles of minimum potential energy and minimum complimentary energy are
More informationExercise: concepts from chapter 8
Reading: Fundamentals of Structural Geology, Ch 8 1) The following exercises explore elementary concepts associated with a linear elastic material that is isotropic and homogeneous with respect to elastic
More informationExample-3. Title. Description. Cylindrical Hole in an Infinite Mohr-Coulomb Medium
Example-3 Title Cylindrical Hole in an Infinite Mohr-Coulomb Medium Description The problem concerns the determination of stresses and displacements for the case of a cylindrical hole in an infinite elasto-plastic
More informationSEMM Mechanics PhD Preliminary Exam Spring Consider a two-dimensional rigid motion, whose displacement field is given by
SEMM Mechanics PhD Preliminary Exam Spring 2014 1. Consider a two-dimensional rigid motion, whose displacement field is given by u(x) = [cos(β)x 1 + sin(β)x 2 X 1 ]e 1 + [ sin(β)x 1 + cos(β)x 2 X 2 ]e
More informationA non-linear elastic/perfectly plastic analysis for plane strain undrained expansion tests
Bolton, M. D. & Whittle, R. W. (999). GeÂotechnique 49, No., 33±4 TECHNICAL NOTE A non-linear elastic/perfectly plastic analysis for plane strain undrained expansion tests M. D. BOLTON and R. W. WHITTLE{
More informationChapter 7. Highlights:
Chapter 7 Highlights: 1. Understand the basic concepts of engineering stress and strain, yield strength, tensile strength, Young's(elastic) modulus, ductility, toughness, resilience, true stress and true
More informationNORMAL STRESS. The simplest form of stress is normal stress/direct stress, which is the stress perpendicular to the surface on which it acts.
NORMAL STRESS The simplest form of stress is normal stress/direct stress, which is the stress perpendicular to the surface on which it acts. σ = force/area = P/A where σ = the normal stress P = the centric
More informationAvailable online at ScienceDirect. Procedia Engineering 144 (2016 )
Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 144 (016 ) 170 177 1th International Conference on Vibration Problems, ICOVP 015 Propagation of Torsional Surface Wave in Anisotropic
More informationFundamentals of Linear Elasticity
Fundamentals of Linear Elasticity Introductory Course on Multiphysics Modelling TOMASZ G. ZIELIŃSKI bluebox.ippt.pan.pl/ tzielins/ Institute of Fundamental Technological Research of the Polish Academy
More informationQuestions Chapter 23 Gauss' Law
Questions Chapter 23 Gauss' Law 23-1 What is Physics? 23-2 Flux 23-3 Flux of an Electric Field 23-4 Gauss' Law 23-5 Gauss' Law and Coulomb's Law 23-6 A Charged Isolated Conductor 23-7 Applying Gauss' Law:
More informationChapter Two: Mechanical Properties of materials
Chapter Two: Mechanical Properties of materials Time : 16 Hours An important consideration in the choice of a material is the way it behave when subjected to force. The mechanical properties of a material
More informationLocalization in Undrained Deformation
Localization in Undrained Deformation J. W. Rudnicki Dept. of Civil and Env. Engn. and Dept. of Mech. Engn. Northwestern University Evanston, IL 621-319 John.Rudnicki@gmail.com Fourth Biot Conference on
More informationSemi-Membrane and Effective Length Theory of Hybrid Anisotropic Materials
International Journal of Composite Materials 2017, 7(3): 103-114 DOI: 10.5923/j.cmaterials.20170703.03 Semi-Membrane and Effective Length Theory of Hybrid Anisotropic Materials S. W. Chung 1,*, G. S. Ju
More information3D Elasticity Theory
3D lasticity Theory Many structural analysis problems are analysed using the theory of elasticity in which Hooke s law is used to enforce proportionality between stress and strain at any deformation level.
More informationMechanics of Materials II. Chapter III. A review of the fundamental formulation of stress, strain, and deflection
Mechanics of Materials II Chapter III A review of the fundamental formulation of stress, strain, and deflection Outline Introduction Assumtions and limitations Axial loading Torsion of circular shafts
More informationTuesday, February 11, Chapter 3. Load and Stress Analysis. Dr. Mohammad Suliman Abuhaiba, PE
1 Chapter 3 Load and Stress Analysis 2 Chapter Outline Equilibrium & Free-Body Diagrams Shear Force and Bending Moments in Beams Singularity Functions Stress Cartesian Stress Components Mohr s Circle for
More informationPlasticity R. Chandramouli Associate Dean-Research SASTRA University, Thanjavur
Plasticity R. Chandramouli Associate Dean-Research SASTRA University, Thanjavur-613 401 Joint Initiative of IITs and IISc Funded by MHRD Page 1 of 9 Table of Contents 1. Plasticity:... 3 1.1 Plastic Deformation,
More informationLarge bending deformations of pressurized curved tubes
Arch. Mech., 63, 5 6, pp. 57 56, Warszawa Large bending deformations of pressurized curved tubes A. M. KOLESNIKOV Theory of Elasticity Department Southern Federal University Rostov-on-Don, 344, Russian
More informationUnsteady Flow of a Newtonian Fluid in a Contracting and Expanding Pipe
Unsteady Flow of a Newtonian Fluid in a Contracting and Expanding Pipe T S L Radhika**, M B Srinivas, T Raja Rani*, A. Karthik BITS Pilani- Hyderabad campus, Hyderabad, Telangana, India. *MTC, Muscat,
More informationChapter 5 Torsion STRUCTURAL MECHANICS: CE203. Notes are based on Mechanics of Materials: by R. C. Hibbeler, 7th Edition, Pearson
STRUCTURAL MECHANICS: CE203 Chapter 5 Torsion Notes are based on Mechanics of Materials: by R. C. Hibbeler, 7th Edition, Pearson Dr B. Achour & Dr Eng. K. El-kashif Civil Engineering Department, University
More informationStability of Thick Spherical Shells
Continuum Mech. Thermodyn. (1995) 7: 249-258 Stability of Thick Spherical Shells I-Shih Liu 1 Instituto de Matemática, Universidade Federal do Rio de Janeiro Caixa Postal 68530, Rio de Janeiro 21945-970,
More informationDiscrete Element Modelling of a Reinforced Concrete Structure
Discrete Element Modelling of a Reinforced Concrete Structure S. Hentz, L. Daudeville, F.-V. Donzé Laboratoire Sols, Solides, Structures, Domaine Universitaire, BP 38041 Grenoble Cedex 9 France sebastian.hentz@inpg.fr
More informationBasic concepts to start Mechanics of Materials
Basic concepts to start Mechanics of Materials Georges Cailletaud Centre des Matériaux Ecole des Mines de Paris/CNRS Notations Notations (maths) (1/2) A vector v (element of a vectorial space) can be seen
More informationConstitutive models: Incremental plasticity Drücker s postulate
Constitutive models: Incremental plasticity Drücker s postulate if consistency condition associated plastic law, associated plasticity - plastic flow law associated with the limit (loading) surface Prager
More informationThermal load-induced notch stress intensity factors derived from averaged strain energy density
Available online at www.sciencedirect.com Draft ScienceDirect Draft Draft Structural Integrity Procedia 00 (2016) 000 000 www.elsevier.com/locate/procedia 21st European Conference on Fracture, ECF21, 20-24
More informationElastic plastic bending of stepped annular plates
Applications of Mathematics and Computer Engineering Elastic plastic bending of stepped annular plates JAAN LELLEP University of Tartu Institute of Mathematics J. Liivi Street, 549 Tartu ESTONIA jaan.lellep@ut.ee
More informationModule 7: Micromechanics Lecture 34: Self Consistent, Mori -Tanaka and Halpin -Tsai Models. Introduction. The Lecture Contains. Self Consistent Method
Introduction In this lecture we will introduce some more micromechanical methods to predict the effective properties of the composite. Here we will introduce expressions for the effective properties without
More informationMassachusetts Institute of Technology 22.68J/2.64J Superconducting Magnets. February 27, Lecture #4 Magnetic Forces and Stresses
Massachusetts Institute of Technology.68J/.64J Superconducting Magnets February 7, 003 Lecture #4 Magnetic Forces and Stresses 1 Forces For a solenoid, energy stored in the magnetic field acts equivalent
More informationSTRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS
1 UNIT I STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define: Stress When an external force acts on a body, it undergoes deformation. At the same time the body resists deformation. The
More information3 2 6 Solve the initial value problem u ( t) 3. a- If A has eigenvalues λ =, λ = 1 and corresponding eigenvectors 1
Math Problem a- If A has eigenvalues λ =, λ = 1 and corresponding eigenvectors 1 3 6 Solve the initial value problem u ( t) = Au( t) with u (0) =. 3 1 u 1 =, u 1 3 = b- True or false and why 1. if A is
More informationMechanics of Materials and Structures
Journal of Mechanics of Materials and Structures ON TORSIONAL VIBRATIONS OF INFINITE HOLLOW POROELASTIC CYLINDERS M. Tajuddin and S. Ahmed Shah Volume 2, Nº 1 January 27 mathematical sciences publishers
More information16.20 HANDOUT #2 Fall, 2002 Review of General Elasticity
6.20 HANDOUT #2 Fall, 2002 Review of General Elasticity NOTATION REVIEW (e.g., for strain) Engineering Contracted Engineering Tensor Tensor ε x = ε = ε xx = ε ε y = ε 2 = ε yy = ε 22 ε z = ε 3 = ε zz =
More informationAn Analytical Model for Long Tube Hydroforming in a Square Cross-Section Die Considering Anisotropic Effects of the Material
Journal of Stress Analysis Vol. 1, No. 2, Autumn Winter 2016-17 An Analytical Model for Long Tube Hydroforming in a Square Cross-Section Die Considering Anisotropic Effects of the Material H. Haghighat,
More informationMechanical Design in Optical Engineering
Torsion Torsion: Torsion refers to the twisting of a structural member that is loaded by couples (torque) that produce rotation about the member s longitudinal axis. In other words, the member is loaded
More informationTheory of Plasticity. Lecture Notes
Theory of Plasticity Lecture Notes Spring 2012 Contents I Theory of Plasticity 1 1 Mechanical Theory of Plasticity 2 1.1 Field Equations for A Mechanical Theory.................... 2 1.1.1 Strain-displacement
More informationTorsional Buckling of Double-Walled Carbon Nanotubes
Torsional Buckling of Double-Walled Carbon Nanotubes S. H. Soong Engineering Science Programme, National University of Singapore Kent Ridge, Singapore 119260 ABSTRACT This paper is concerned with the torsional
More informationApplication of piezoelectric actuators to active control of composite spherical caps
Smart Mater. Struct. 8 (1999 18. Printed in the UK PII: S964-176(991661-4 Application of piezoelectric actuators to active control of composite spherical caps Victor Birman, Gareth J Knowles and John J
More informationExpansion of circular tubes by rigid tubes as impact energy absorbers: experimental and theoretical investigation
Expansion of circular tubes by rigid tubes as impact energy absorbers: experimental and theoretical investigation M Shakeri, S Salehghaffari and R. Mirzaeifar Department of Mechanical Engineering, Amirkabir
More informationMechanics of Materials and Structures
Journal of Mechanics of Materials and Structures ON SMALL AZIMUTHAL SHEAR DEFORMATION OF FIBRE-REINFORCED CYLINDRICAL TUBES Mohamed A. Dagher and Kostas P. Soldatos Volume 6, No. 1-4 January June 2011
More informationCHAPTER THREE SYMMETRIC BENDING OF CIRCLE PLATES
CHAPTER THREE SYMMETRIC BENDING OF CIRCLE PLATES * Governing equations in beam and plate bending ** Solution by superposition 1.1 From Beam Bending to Plate Bending 1.2 Governing Equations For Symmetric
More informationElements of Continuum Elasticity. David M. Parks Mechanics and Materials II February 25, 2004
Elements of Continuum Elasticity David M. Parks Mechanics and Materials II 2.002 February 25, 2004 Solid Mechanics in 3 Dimensions: stress/equilibrium, strain/displacement, and intro to linear elastic
More informationPrediction of geometric dimensions for cold forgings using the finite element method
Journal of Materials Processing Technology 189 (2007) 459 465 Prediction of geometric dimensions for cold forgings using the finite element method B.Y. Jun a, S.M. Kang b, M.C. Lee c, R.H. Park b, M.S.
More informationUNLOADING OF AN ELASTIC-PLASTIC LOADED SPHERICAL CONTACT
2004 AIMETA International Tribology Conference, September 14-17, 2004, Rome, Italy UNLOADING OF AN ELASTIC-PLASTIC LOADED SPHERICAL CONTACT Yuri KLIGERMAN( ), Yuri Kadin( ), Izhak ETSION( ) Faculty of
More informationFinite element Analysis of thermo mechanical stresses of two layered composite cylindrical pressure vessel
Finite element Analysis of thermo mechanical stresses of two layered composite cylindrical pressure vessel Arnab Choudhury *1, Samar Chandra Mondol #2, Susenjit Sarkar #3 *Faculty, Mechanical Engineering
More information4. BEAMS: CURVED, COMPOSITE, UNSYMMETRICAL
4. BEMS: CURVED, COMPOSITE, UNSYMMETRICL Discussions of beams in bending are usually limited to beams with at least one longitudinal plane of symmetry with the load applied in the plane of symmetry or
More informationThe Ultimate Load-Carrying Capacity of a Thin-Walled Shuttle Cylinder Structure with Cracks under Eccentric Compressive Force
The Ultimate Load-Carrying Capacity of a Thin-Walled Shuttle Cylinder Structure with Cracks under Eccentric Compressive Force Cai-qin Cao *, Kan Liu, Jun-zhe Dong School of Science, Xi an University of
More information16.21 Techniques of Structural Analysis and Design Spring 2003 Unit #5 - Constitutive Equations
6.2 Techniques of Structural Analysis and Design Spring 2003 Unit #5 - Constitutive quations Constitutive quations For elastic materials: If the relation is linear: Û σ ij = σ ij (ɛ) = ρ () ɛ ij σ ij =
More informationHomework 4 PHYS 212 Dr. Amir
Homework 4 PHYS Dr. Amir. (I) A uniform electric field of magnitude 5.8 passes through a circle of radius 3 cm. What is the electric flux through the circle when its face is (a) perpendicular to the field
More informationGauss s Law. Chapter 22. Electric Flux Gauss s Law: Definition. Applications of Gauss s Law
Electric Flux Gauss s Law: Definition Chapter 22 Gauss s Law Applications of Gauss s Law Uniform Charged Sphere Infinite Line of Charge Infinite Sheet of Charge Two infinite sheets of charge Phys 2435:
More informationDAMPING OF GENERALIZED THERMO ELASTIC WAVES IN A HOMOGENEOUS ISOTROPIC PLATE
Materials Physics and Mechanics 4 () 64-73 Received: April 9 DAMPING OF GENERALIZED THERMO ELASTIC WAVES IN A HOMOGENEOUS ISOTROPIC PLATE R. Selvamani * P. Ponnusamy Department of Mathematics Karunya University
More informationUnit I Stress and Strain
Unit I Stress and Strain Stress and strain at a point Tension, Compression, Shear Stress Hooke s Law Relationship among elastic constants Stress Strain Diagram for Mild Steel, TOR steel, Concrete Ultimate
More informationThe effect of rigidity on torsional vibrations in a two layered poroelastic cylinder
Int. J. Adv. Appl. Math. and Mech. 3(1) (2015) 116 121 (ISSN: 2347-2529) Journal homepage: www.ijaamm.com International Journal of Advances in Applied Mathematics and Mechanics The effect of rigidity on
More information20. Rheology & Linear Elasticity
I Main Topics A Rheology: Macroscopic deformation behavior B Linear elasticity for homogeneous isotropic materials 10/29/18 GG303 1 Viscous (fluid) Behavior http://manoa.hawaii.edu/graduate/content/slide-lava
More informationS.P. Timoshenko Institute of Mechanics, National Academy of Sciences, Department of Fracture Mechanics, Kyiv, Ukraine
CALCULATION OF THE PREFRACTURE ZONE AT THE CRACK TIP ON THE INTERFACE OF MEDIA A. Kaminsky a L. Kipnis b M. Dudik b G. Khazin b and A. Bykovtscev c a S.P. Timoshenko Institute of Mechanics National Academy
More informationA Notes Formulas. This chapter is composed of 15 double pages which list, with commentaries, the results for:
The modeling process is a key step of conception. First, a crude modeling allows to validate (or not) the concept and identify the best combination of properties that maximize the performances. Then, a
More informationChapter 3. Load and Stress Analysis. Lecture Slides
Lecture Slides Chapter 3 Load and Stress Analysis 2015 by McGraw Hill Education. This is proprietary material solely for authorized instructor use. Not authorized for sale or distribution in any manner.
More informationEffect of embedment depth and stress anisotropy on expansion and contraction of cylindrical cavities
Effect of embedment depth and stress anisotropy on expansion and contraction of cylindrical cavities Hany El Naggar, Ph.D., P. Eng. and M. Hesham El Naggar, Ph.D., P. Eng. Department of Civil Engineering
More informationNumerical analysis for an interpretation of the pressuremeter test in cohesive soil
Numerical analysis for an interpretation of the pressuremeter test in cohesive soil J. Monnet Joseph Fourier University L3S-R Domaine Universitaire, BP n 53, 3841, Grenoble, Cedex 9, France jmonnet@ujf-grenoble.fr
More informationMidterm Examination. Please initial the statement below to show that you have read it
EN75: Advanced Mechanics of Solids Midterm Examination School of Engineering Brown University NAME: General Instructions No collaboration of any kind is permitted on this examination. You may use two pages
More informationweek 3 chapter 28 - Gauss s Law
week 3 chapter 28 - Gauss s Law Here is the central idea: recall field lines... + + q 2q q (a) (b) (c) q + + q q + +q q/2 + q (d) (e) (f) The number of electric field lines emerging from minus the number
More information202 Index. failure, 26 field equation, 122 force, 1
Index acceleration, 12, 161 admissible function, 155 admissible stress, 32 Airy's stress function, 122, 124 d'alembert's principle, 165, 167, 177 amplitude, 171 analogy, 76 anisotropic material, 20 aperiodic
More information6.1 Formulation of the basic equations of torsion of prismatic bars (St. Venant) Figure 6.1: Torsion of a prismatic bar
Module 6 Torsion Learning Objectives 6.1 Formulation of the basic equations of torsion of prismatic bars (St. Venant) Readings: Sadd 9.3, Timoshenko Chapter 11 e e 1 e 3 Figure 6.1: Torsion of a prismatic
More informationHomework Problems. ( σ 11 + σ 22 ) 2. cos (θ /2), ( σ θθ σ rr ) 2. ( σ 22 σ 11 ) 2
Engineering Sciences 47: Fracture Mechanics J. R. Rice, 1991 Homework Problems 1) Assuming that the stress field near a crack tip in a linear elastic solid is singular in the form σ ij = rλ Σ ij (θ), it
More informationModule 6: Stresses around underground openings. 6.2 STRESSES AROUND UNDERGROUND OPENING contd.
LECTURE 0 6. STRESSES AROUND UNDERGROUND OPENING contd. CASE : When σ x = 0 For σ x = 0, the maximum tangential stress is three times the applied stress and occurs at the boundary on the X-axis that is
More informationTorsion Stresses in Tubes and Rods
Torsion Stresses in Tubes and Rods This initial analysis is valid only for a restricted range of problem for which the assumptions are: Rod is initially straight. Rod twists without bending. Material is
More informationME Final Exam. PROBLEM NO. 4 Part A (2 points max.) M (x) y. z (neutral axis) beam cross-sec+on. 20 kip ft. 0.2 ft. 10 ft. 0.1 ft.
ME 323 - Final Exam Name December 15, 2015 Instructor (circle) PROEM NO. 4 Part A (2 points max.) Krousgrill 11:30AM-12:20PM Ghosh 2:30-3:20PM Gonzalez 12:30-1:20PM Zhao 4:30-5:20PM M (x) y 20 kip ft 0.2
More informationEnd forming of thin-walled tubes
Journal of Materials Processing Technology 177 (2006) 183 187 End forming of thin-walled tubes M.L. Alves a, B.P.P. Almeida b, P.A.R. Rosa b, P.A.F. Martins b, a Escola Superior de Tecnologia e Gestão
More informationParametric Study Of The Material On Mechanical Behavior Of Pressure Vessel
Parametric Study Of The Material On Mechanical Behavior Of Pressure Vessel Dr. Mohammad Tariq Assistant Professor Mechanical Engineering Department SSET, SHIATS-Deemed University, Naini, Allahabad, U.P.,
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 informationPhysics Lecture: 09
Physics 2113 Jonathan Dowling Physics 2113 Lecture: 09 Flux Capacitor (Schematic) Gauss Law II Carl Friedrich Gauss 1777 1855 Gauss Law: General Case Consider any ARBITRARY CLOSED surface S -- NOTE: this
More informationYou may not start to read the questions printed on the subsequent pages until instructed to do so by the Invigilator.
MATHEMATICAL TRIPOS Part III Thursday 1 June 2006 1.30 to 4.30 PAPER 76 NONLINEAR CONTINUUM MECHANICS Attempt FOUR questions. There are SIX questions in total. The questions carry equal weight. STATIONERY
More informationChapter 21 Chapter 23 Gauss Law. Copyright 2014 John Wiley & Sons, Inc. All rights reserved.
Chapter 21 Chapter 23 Gauss Law Copyright 23-1 What is Physics? Gauss law relates the electric fields at points on a (closed) Gaussian surface to the net charge enclosed by that surface. Gauss law considers
More information