The nonaxisymmetric thermostressed state of laminated isotropic and rectilinearly orthotropic solids of revolution

A technique for determination of the nonaxisymmetric elastoplastic stress-strain state of laminated isotropic and rectilinearly orthotropic solids of revolution under nonisothermal loading is described. The semianalytic method of finite elements is used together with the method of successive approximations. The deformation of isotropic materials is described by the equations of the theory of deformation along trajectories of small curvature, and the deformation of orthotropic materials is described by the equations of the theory of elasticity. The thermostressed state of a three-layered solid of revolution of complex form made from isotropic and cylindrically and rectilinearly orthotropic materials subject to nonaxisymmetric heating is studied. S. P. Timoshenko Institute of Mechanics, National Academy of Sciences of Ukraine, Kiev. Translated from Prikladnaya Mekhanika, Vol. 36, No. 4, pp. 88–95, April, 2000.     

The nonaxisymmetric elastoplastic state of isotropic and cylindrically orthotropic solids of revolution under nonisothermal loading

A technique for numerical analysis of the nonaxisymmetric elastoplastic stress-strain state of laminated isotropic and cylindrically orthotropic bodies of revolution under nonisothermal loading with allowance for its history is stated. The strain of isotropic materials is described by the equations of the theory of strain along small-curvature trajectories, while Hooke's law is used to describe the strain of orthotropic materials. The necessity of accounting for the loading history is shown by an example of a nonaxisymmetrically heated sandwich solid of revolution. S. P. Timoshenko Institute of Mechanics, National Academy of Sciences of Ukraine, Kiev. Translated from Prikladnaya Mekhanika, Vol. 36, No. 2, pp. 83–90, February, 2000.     

THE GENERALIZED GALERKIN’S EQUATION OF THE FINITE ELEMENT,THE BOUNDARY VARIATIONAL EQUATIONS AND THE BOUNDARY INTEGRAL EQUATIONS

Based on[1 ],we have further applied the variational princi-ple of the variable boundary to investigate the discretizationanalysis of the solid system and derived the generalized Ga-lerkin’s equations of the finite element.the boundary varia-tional equations and the boundary integral equations.These e-quations indicate that the unknown functions of the solid sys-tem must satisfy the conditions in the element S_a or on the boun-dariesГ_a.These equations are applied to establishing the discreti-zation equations in order to obtain the numerical solution ofthe unknown functions.At a time these equations can be usedas the basis for the simplified calculation in various corres-ponding cases.In this paper,the results of boundary integral equationsshow that the calculation of integration is not accurate alongthe surfaceГ_a of interior element S_a by J-integral suggestedby Rice[2].     

A spectral–finite difference solution of the Navier–Stokes equations in three dimensions

A new computational code for the numerical integration of the three-dimensional Navier–Stokes equations in their non-dimensional velocity–pressure formulation is presented. The system of non-linear partial differential equations governing the time-dependent flow of a viscous incompressible fluid in a channel is managed by means of a mixed spectral–finite difference method, in which different numerical techniques are applied: Fourier decomposition is used along the homogeneous directions, second-order Crank–Nicolson algorithms are employed for the spatial derivatives in the direction orthogonal to the solid walls and a fourth-order Runge–Kutta procedure is implemented for both the calculation of the convective term and the time advancement. The pressure problem, cast in the Helmholtz form, is solved with the use of a cyclic reduction procedure. No-slip boundary conditions are used at the walls of the channel and cyclic conditions are imposed at the other boundaries of the computing domain. Results are provided for different values of the Reynolds number at several time steps of integration and are compared with results obtained by other authors. © 1998 John Wiley & Sons, Ltd.     

Decomposition of an axisymmetric body of revolution made of a material of complex chemical composition in a partially ionized airstream

The problem of the decomposition of an axisymmetric body of revolution in an ionized airstteam is formulated and solved numerically. Equations are presented for numerical calculation of the diffusional fluxes for generalized Schmidt numbers for the case of ambipolar diffusion in a multicomponent partially ionized mixture with ions of various sorts which differ in mass and charge. For materials consisting of the elements H, C, N, and O we discuss the kinetic decomposition condition, which is used to close the system of boundary conditions, in the form of the dependence of the linear decomposition rate on the surface temperature, gas pressure, and body dimensions. As an example we calculate the decomposition of a sphere made from a material which is similar in properties to textolite in an airstream with stagnation temperature of 14 000° K. It is found that the distribution of the decomposition rate over the sphere surface is nearly independent of the type of material and freestream parameters and coincides to within 10 percent with the distribution of the thermal fluxes to the nondecomposed body. We study a generalized analogy for the mass transfer coefficients in the vicinity of the forward stagnation point.In conclusion the authors wish to thank O. N. Suslov for numerous valuable comments.     

脆性固体碎裂过程中的最快卸载特性

脆性固体在高应变率拉伸过程中常破碎为多块碎片.论文通过一个一维理论模型,研究动态脆性碎裂过程中固体内部载荷卸载规律,以及碎片尺度的计算方法.假设一维固体中裂纹等间距分布、同时起裂,研究均匀应变率拉伸作用下裂纹阵列的扩张过程.采用线弹性波动方程组描述未断裂固体的动力学关系,采用粘滞断裂模型(cohesive fracture model)描述裂纹的扩张行为,形成完整的初边值问题.采用沿特征线的有限差分计算格式求解控制方程组,得到固体在碎裂过程不同时刻下单位裂纹体内部的应力分布曲线,以及单位裂纹体平均应力随时间的变化规律,确定单位裂纹体达到完全断裂所需要的时间.在给定应变率下,分析不同裂纹间距下的碎裂卸载时间,以及使单位裂纹体以最快速度完全卸载所对应的最佳裂纹间距,并以此间距估算脆性固体在自然动态碎裂过程中的平均碎片尺度.进一步研究了具有不同粘滞性断裂特性的脆性固体的碎片尺度计算数值的差异.     

A class of elastic-plastic stress distributions

Similarity methods are used to find solutions to the equations governing elastic-plastic torsion of a solid of revolution. The solutions are expressed in terms of integrals of two ordinary differential equations.     

An iteration method for integral equations arising from axisymmetric loading problems

Let the concentrated forces and the centers of pressure with unknown density functions x(ξ) and y(ξ) respectively be distributed along the axis z outside the solid, then one can reduce an axismmetric loading problem of solids of revolution to two simultaneous Fredholm integral equations. An iteration method for solving such equations is duscussed. A lemma equivalent to E. Rakotch’s contractive mapping theorem and a theorem concerning the convergent proof of the iteration method are presented.     

FLAT-PLATE BOUNDARY-LAYER FLOWS INDUCED BY DUSTY SHOCK WAVE

ＦＬＡＴ－ＰＬＡＴＥＢＯＵＮＤＡＲＹ－ＬＡＹＥＲＦＬＯＷＳＩＮＤＵＣＥＤＢＹＤＵＳＴＹＳＨＯＣＫＷＡＶＥ（王柏懿）（陶锋）ＦＬＡＴ－ＰＬＡＴＥＢＯＵＮＤＡＲＹ－ＬＡＹＥＲＦＬＯＷＳＩＮＤＵＣＥＤＢＹＤＵＳＴＹＳＨＯＣＫＷＡＶＥ￥ＷａｎｇＢｏｙｉ；Ｔａ...     

前屈曲应力状态对组合加肋旋转壳失稳临界压力影响的探讨

推导了包含前屈曲弯矩和横剪力的旋转壳弹性稳定性基本方程.运用Riccati传递矩阵法对组合加肋旋转壳算例进行了稳定性分析,并与假设前屈曲状态为薄膜应力状态计算出的失稳临界压力进行了比较.结果表明,前屈曲弯矩和横剪力对组合加肋旋转壳失稳临界压力的影响较小,随着壳板厚度和肋骨尺寸的增大及肋骨间距的缩短,影响略有增大.因而,分析组合加肋旋转壳弹性稳定性时,前屈曲状态采用薄膜应力状态的假设是合理的.     

Non-linear static and dynamic deformations of shells of revolution†

The rate equation method, previously developed by the authors, is extended to the analysis of static and dynamic finite deformations of shells of revolution. As an example of the technique, the static and dynamic response of an initially flat plate under spatially uniform, but time varying pressure, is analyzed. Full non-linear shell equations are used in the analysis, and results are presented for large static deflections as well as for large amplitude free and forced vibrations.

The accuracy of the rate equation method is verified by comparison with known solutions obtained by other methods. This comparison also establishes the superiority of the rate equation method over other existing methods as far as calculation times and computer storage requirements are concerned.     

Universal equations for the laminar boundary layer on a solid of revolution in an oblique gas flow

We consider the problem of laminar gas motion in the boundary layer on a solid of revolution oriented at an angle of attack. The parametric method of L. G. Loitsyanskii is used for the solution. The effect of the external current and the form of the body are considered by introduction of three series of parameters. A corresponding system of universal equations is obtained, which is then numerically integrated over a wide range of parameters and their combinations. The results permit evaluation of the general principles of flow in a boundary layer on a solid of revolution in an oblique gas flow.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 32–41, July–August, 1973.     

Thermoelastoplastic State of Flexible Laminated Shells under Axisymmetric Loading Along Various Plane Paths

The paper presents a technique for thermoelastoplastic stress–strain analysis of flexible laminated shells of revolution under complex axisymmetric loading. The constitutive deformation equations are used to describe loading along arbitrary plane paths. The problem is solved by the method of successive approximations. A numerical example is given     

Determining the Axisymmetric Geometrically Nonlinear Thermoviscoelastoplastic State of Laminated Shells by the Theory of Deformation Along Paths of Small Curvature

A technique is developed for determining the thermoviscoelastoplastic geometrically nonlinear axisymmetric stress–strain state of laminar shells of revolution under loads that induce meridional stress and torsion. The technique is based on the hypotheses of rectilinear element for the whole stack of layers. The relations of the theory of deformations along paths of small curvature are used as equations of state. The solution is reduced to the numerical integration of a system of ordinary differential equations. The technique is tried out by a test example and illustrated by determining the geometrically nonlinear thermoviscoelastoplastic state of a corrugated shell     

Describing the thermoelastoplastic deformation of compound shells under axisymmetric loading with allowance for the third invariant of the stress deviator

The paper outlines a procedure for the numerical analysis of the thermoelastoplastic stress–strain state of thin compound shells of revolution under axisymmetric nonisothermal loading. The constitutive equations describing the thermoelastoplastic deformation of isotropic materials along paths of small curvature and incorporating the third invariant of the stress deviator are used. A numerical example is presented     

On the application of mixed method to solve solids of revolution with discrete fixed supports

In this paper, the force method of statically indeterminate structure mechanics is used to treat the solids of revolution with discrete fixed supports. The reactionary forces of discrete fixed supports are considered as statically indeterminate unknown variables. The force-method canonical equations, in which the coefficient matrix and the right-hand vector are computed by semi-analytical finite element method, are solved. Then the finite element solution of solid of revolution with discrete fixed supports is calculated with the external loads superposed from the assigned external loads and the reactionary forces of discrete supports.     

Vortex Scattering of Monatomic Gas Along Plane Curves

An invariant submodel of gas dynamics equations constructed on a three-dimensional subalgebra with a projective operator for the case of monatomic gas is under consideration. The submodel is reduced to an Abel equation, with integral curves constructed for it. For a separatrix of a saddle, an approximate solution is studied. Such solutions describe the vortex scattering of gas along plane curves placed on the surface of revolution.     

Determining the Thermoviscoplastic State of Shells of Revolution Subject to Creep Damage

A technique is developed for determining the thermoviscoplastic state of shells of revolution with allowance for creep damage. The technique is based on the hypotheses of rectilinear element and the theory of deformation along paths of small curvature. The equivalent stress appearing in the kinetic equations of damage and creep is determined using a creep-rupture criterion that accounts for the stress mode and the level of irreversible strains. The technique is tested by determining the thermoviscoplastic state and time to failure of tubular specimens under a tensile force and a torque     

Numerical modelling of the stability of loaded shells of revolution containing fluid flows

A mixed finite-element algorithm is proposed to study the dynamic behavior of loaded shells of revolution containing a stationary or moving compressible fluid. The behavior of the fluid is described by potential theory, whose equations are reduced to integral form using the Galerkin method. The dynamics of the shell is analyzed with the use of the variational principle of possible displacements, which includes the linearized Bernoulli equation for calculating the hydrodynamic pressure exerted on the shell by the fluid. The solution of the problem reduces to the calculation and analysis of the eigenvalues of the coupled system of equations. As an example, the effect of hydrostatic pressure on the dynamic behavior of shells of revolution containing a moving fluid is studied under various boundary conditions. __________ Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 49, No. 2, pp. 185–195, March–April, 2008