Deformation and fracture of crystalline materials under complex loading-program conditions

In predicting the deformation and conditions of fracture of materials under complex loading program conditions one must consider the entire duration of the deformation process.The problem becomes complicated in cases of a simultaneous operation of various mechanisms of deformation and fracture, e. g., when plastic deformation is superposed (once or repeatedly) on creep.A promising phenomenological approach to this problem may be based on concepts of the mechanical equation of state of materials. A hypothesis of the existence of the equation of state depending on a finite number of structural parameters was formulated by Kröner [1] for the case of the three-dimensional law of plasticity and by Rabotnov [2] for the case of creep and fracture under uniaxial stress state conditions.This article is concerned with the application of the hypothesis of the mechanical equation of state to the problem of deformation and fracture of materials (in the uniaxial case) under complex loading program conditions.     

Material model describing the orientation dependent creep behavior of single crystals based on dislocation densities of slip systems

A material model is proposed which describes single crystal creep behavior by evolution equations for dislocation densities on individual slip systems. An interaction matrix determines the influence from one glide system to the other. Assuming a face centered cubic crystal, allowing deformation on octahedral glide planes and cube glide planes with a Burgers vector of the type a/2〈110〉, nine independent parameters of the interaction matrix can be distinguished. A parameter check of the nine independent parameters has been carried out, showing the influence of parameters on specific orientations of the load axis. If one assumes dislocation interaction of a glide system only with itself a smooth behavior is predicted with a maximum creep rate for [001] orientation, followed by [011] and [111]. If a strong interaction is assumed, the orientation dependent creep behavior is not at all smooth, instead it shows a sharp drop in creep rates mainly in symmetric positions of the standard orientation triangle. The orientations with highest creep rates are in this case those which favor single glide. Highly symmetric orientations, such as [001], [011] and [111] have strongly decreased stationary creep rates.     

Transient behaviour of the mechanical loss factor of high density polyethylene during creep and relaxation

The mechanical loss factor of high density polyethylene has been measured during creep and stress relaxation experiments. The application of a constant stress (creep) or strain (relaxation) resulted in an instantaneous increase in tan above the value obtained in absence of the creep or relaxation process. During the flow the tan-value decreased and approached an apparent equilibrium value slightly above the value obtained without the static load or deformation. This behaviour was observed both at 1 and 10 Hz and at 23 and 60 °C. It is suggested that this time dependence of the mechanical loss factor is associated with the basic mechanisms responsible for the creep or relaxation process itself.     

The finite deflection equations of anisotropic laminated shallow shells

In this paper, basing on ref. [1] we improved and extended that which is concerned with a view of investigating the finite deflection equations of anisotropic laminated shallow shells subjected to static loads, dynamic loads and thermal loads. We have considered the most general bending-stretching couplings and the shear deformations in the thickness direction, and derived the equilibrium equations, boundary conditions and initial conditions. The differential equations expressed in terms of generalized displacements u₀, ₀ and are obtained. From them, we could solve the problems of stress analysis, deformation, stability and vibration. For some commonly encountered cases, we derived the simplified equations and methods.     

A study on the stability of blood vessels

The paper deals with an analytical study on the stability of blood vessel walls. The theory of small deformation superposed on a known state of finite deformation, together with the anisotropic visco-elastic constitutive relations of Vaishnav and Patel [1] for vascular tissues, are employed for the purpose. By using the material functions of Young et al. [2], the latent instabilities of canine middle descending thoracic aortic wall are predicted in terms of the circumferential and axial extension ratios.Paper presented by J. C. Misra at the Fourth International Congress of Biorheology, Jikei University School of Medicine, Tokyo (Japan), July 27–August 1, 1981.     

Deformation and Failure of Aluminum Alloys from the Standpoint of the Kinetic Concept of Strength

A thermalactivation analysis was performed of experimental data on the strain and failure of 1201 T1, D16 T, and AK41 T1 aluminum alloys. The experiments were conducted under constant loads in creep conditions and under increasing loads. The duration of the tests was varied from fractions of a second to ten thousand hours, and the temperature ranged from 77 to 473 K. The rate activation parameters in the equations of steadystate creep and plastic strain were determined. Information was obtained on the relationship between plastic strain and failure. The plastic strain rate is shown to be affected by relaxation phenomena. The plastic characteristics of the alloys and their dependences on the temperature and time to failure are given.     

Kinetic Approach to Prediction of the Life of Aluminum Alloys under Various Thermal–Temporal Loading Conditions

Results of investigation of the life of D16 T, AK41 T1, and 1201 T1 aluminum alloys are generalized on the basis of the kinetic concept of failure. The life is studied under creep at constant loads and loads increasing with different rates and at different temperatures. The temperature is varied within the range of 473–77 K, and the duration of tests ranges from fractions of a second to ten thousand hours. Information on the effect of internalstress relaxation on the life of alloys is obtained. A method for predicting the life with allowance for relaxation processes in solids is verified experimentally.     

Dissipative instability of a nonisothermal electrically conducting flow between parallel plates in a transverse magnetic field

Problems of dissipative instability (in particular, overheating) in magnetohydrodynamies has been studied in [1–6]. The Leontovieh mechanism of overheating instability is explained in [I] by the example of a stationary homogeneous plasma in a strong magnetic field along which current flows. The rate of buildup of perttbations is estimated in [2] to explain the effect of overheating instability on the operation of an MHD generator. The effect of inhomogeneity in the temperature field and in the boundaries of the region on the formarion of this instability has been studied by the example of discharge in a stationary medium in the absence of a magnetic field [3], Certain cases of overheating instability in magnetohydrodynamies are considered in [4, 6], where it is shown that it can be aperiodic as well as oseillatery (Alfven and acoustic waves). Finally, the hydro-dynamic and overheating branches of instability in the ease of non-isothermal plasma flow in a plane MHD channel was investigated in [6]. But the overheating instability was examined without allowance for the dependence of the viscosity and thermal-conductivity coefficients on temperature in the limiting case S R_m 1 and only for small perturbation wavelengths. The development of shortwave perturbations is studied below with allowance for viscosity and thermal conductivity and for a wider range of conditions A 1. Overheating instability over the entire range of wavelengths for the ease considered in [6] is also studied.The author thanks Yu. M. Zolotaikin for programming and performing the calculations.     

Finite deformation of elastic membranes with application to the stability of an inflated and extended tube

A theory is formulated for the finite deformation of a thin membrane composed of homogeneous elastic material which is isotropic in its undeformed state. The theory is then extended to the case of a small deformation superposed on a known finite deformation of the membrane. As an example, small deformations of a circular cylindrical tube which has been subjected to a finite homogeneous extension and inflation are considered and the equations governing these small deformations are obtained for an incompressible material. By means of a static analysis the stability of cylindrically symmetric modes for the inflated and extended cylinder with fixed ends is determined and the results are verified by a dynamic analysis. The stability is considered in detail for a Mooney material. Methods are developed to obtain the natural frequencies for axially symmetric free vibrations of the extended and inflated cylindrical membrane. Some of the lower natural frequencies are calculated for a Mooney material and the methods are compared.     

化学固沙结皮力学性能的研究

通过自行设计的实验装置,测量了不同混合比例的化学固沙结皮在不同载荷下的弯曲蠕变。在此基础上,导出化学固沙结皮的弹性模量E和蠕变函数公式,并数值模拟了沙床上的结皮在集中载荷作用下的变形。     

Area rule for integral quantities

In hydrodynamics and aerodynamics there is an area rule for nearly axisymmetric bodies. It states that the drag [1–3], the coefficient of heat transfer and the ablation [4], and also the wake parameters [5] of a three-dimensional body are equal to the analogous quantities for an axisymmetric body which has the same distribution of the cross sectional area along the axis. In some cases, the area rule holds for bodies which depart strongly from axial symmetry [6]. It is shown in the present paper that equality also holds for other integral quantities and not only in hydrodynamic problems.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 157–159, July–August, 1981.We thank Yu. B. Lifshits for helpful comments.     

Elasto‐plastic Hardening and Shakedown of Masonry Arch Joints

The behavior of joints made of sand–lime mortar, such as used in a wide variety of structures from ancient times through the early twentieth century, can be clearly distinguished from the behavior of joints made with hydraulic cement mortar. Experiments on confined mortar specimens have confirmed that the weaker and more ductile sand–lime mortar can be accurately modeled as a Drucker–Prager material with a compression cap and exponential hardening on the cap portion of the yield surface. Joints of sand–lime mortar subject to axial thrust and moment are found experimentally to yield under very small loads, and to follow a linear hardening rule beyond the yield point. This behavior can be replicated analytically using a Drucker–Prager constitutive law with exponential hardening. The yield surface and hardening function for an entire mortar joint are representable by Maier's theory of piecewise linear yield function and interacting yield planes. As a consequence, an arch jointed with sand–lime mortar is found to shake down under moving loads above the yield limit and below the collapse load. The shakedown behavior of a sand–lime mortar jointed masonry arch is confirmed experimentally.Sommario. II comportamento dei giunti realizzati con malta di calce, del tipo di quelli utilizzati in unampia varietà di strutture dall antichità sino allinizio di questo secolo, può essere chiaramente distinto dal comportamento dei giunti realizzati con malta idraulica. Esperimenti condotti su provini confinati di malta hanno infatti evidenziato che il comportamento della malta di calce, meno resistente e più duttile, può essere accuratamente modellato con un materiale di Drucker–Prager, adottando un troncamento della resistenza a compressione ed un incrudimento esponenziale della superficie di snervamento nella porzione troncata. Si è rilevato sperimentalmente che i giunti di malta di calce, soggetti a sforzo assiale e momento flettente, raggiungono lo snervamento sotto carichi molto modesti, e quindi seguono una legge di incrudimento lineare oltre il punto di snervamento. Questo comportamento può essere riprodotto analiticamente utilizzando la legge costitutiva di Drucker–Prager con incrudimento esponenziale. La superficie di snervamento e la funzione di incrudimento per un giunto di malta sono rappresentabili mediante la teoria di Maier delle funzioni di snervamento lineari a tratti e dei piani di snervamento interagenti. Di conseguenza, un arco con giunti di malta di calce perviene alladattamento plastico (shakedown) sotto carichi mobili superiori al limite di snervamento ed inferiori al carico di collasso. Tale raggiungimento della condizione di adattamento plastico di archi di muratura con giunti di malta di calce è confermato sperimentalmente.     

A dynamic moiré method for deformation measurement of curved surfaces

A simple method is proposed for obtaining moiré patterns, and information is given on the deformation of curved surfaces. The experimental arrangement is based on the projection-moiré principle and consists of a projector and a camera. A transparent object, e.g., a shell with line gratings, is projected onto the focal plane of this projector and superposed there with a reference grating which describes the undeformed state of the curved surface in the form of a transparent picture. Moiré patterns are obtained by simultaneously superposing the projected line grating in the shell's deformed state and the reference grating. They present a general picture of the behavior of the object during loading, such as during impact if the patterns are recorded with a high-speed camera.     

A viscoelastic constitutive model of rubber under small oscillatory load superimposed on large static deformation considering the Payne effect

The viscoelastic behavior of carbon-black-filled rubber under small oscillatory loads superimposed on large static deformation is dealt with. In this class of problems, as the strain amplitudes of the load increase, the dynamic stiffness decreases, and this phenomenon is known as the Payne effect. Besides the effects of the static deformation and the frequencies of the superimposed dynamic load, the Payne effect is considered in this study. Influence factors are introduced in this model in order to consider the influence of static predeformation, the dynamic-strain-dependent properties, and frequency-dependent properties. For simplicity, separation of the three dominant variables, frequency, prestatic deformation, and dynamic amplitude of strain, is assumed. The Kraus model is used for describing the Payne effect. Dynamic tension tests are executed to obtain the model parameters and also for the verification of the proposed model. The suggested constitutive equation shows reasonable agreement with test data.     

Parameters of streamer breakdown in xenon

It is known from experiments [1–3] that the velocity of streamers, induced in the center of the interelectrode gap and propagating to the electrodes under conditions when the streamer length is comparable with the distance between the electrodes, increases linearly as the streamer length increases. This relationship is in qualitative agreement with theory [4], Nevertheless, the velocity of streamers starting from the electrodes and propagating in a long interelectrode gap remains practically constant during the whole propagation process [5, 6], In the case of short gaps (2–5 cm), constancy of the velocity is observed during the stage of the process when the length of the streamer is much less (20%) than the length of the gap [7], Since the electric field at its end controls the streamer propagation, the constancy of the streamer velocity indicates that the controlling field is constant under these conditions. A number of theoretical models were proposed in [8–13] which describe uniformly moving anode- and cathode-directed streamers (henceforth called anode and cathode streamers). Comparison of experimental data with the corresponding theoretical model enables one to determine the streamer parameters: the electric field, the charged-particle density, the current density, the channel radius, etc. In the case of an anode streamer in Xe an attempt at such a comparison was made, in particular, in [6]. However, the lack of reliable data on the value of the drift velocity and the diffusion coefficient of electrons in Xe for E/p (10² – 10³) V/cm · mm Hg allowed only rough estimates to be made. In this paper a numerical calculation is made of the drift velocity, the diffusion coefficient of electrons in Xe, and the rate of excitation of Xe atoms in the resonance level in the range of values of E/p (10¹–10³) V cm · mm Hg, and the volt-ampere characteristic of the breakdown is measured under conditions described in [6] (p₀=300 mm Hg and E 10⁴–10⁵ V/cm). Using these results, the formulas for the velocity of anode [12] and cathode [13] streamers, and experimental data [6], the parameters of the streamers studied in [6] are determined.Translated from Zhurnal Prikladnoi Meknaniki i Tekhmcheskoi Fiziki, No. 3, pp. 6–11, May–June, 1976.The authors thank A. T. Rakhimov and A. N. Starostin for useful discussions, and A. V. Markov for help with the experiments.     

A New Shear-Compression Test for Determining the Pressure Influence on the Shear Response of Elastomers

A new shear-compression experiment for investigating the influence of hydrostatic pressure (mean stress) on the large deformation shear response of elastomers is presented. In this new design, a nearly uniform torsional shear strain is superposed on a uniform volumetric compression strain generated by axially deforming specimens confined by a stack of thin steel disks. The new design is effective in applying uniform shear and multiaxial compressive stress on specimens while preventing buckling and barreling during large deformation under high loads. By controlling the applied pressure and shear strain independently of each other, the proposed setup allows for measuring the shear and bulk response of elastomers at arbitrary states within the shear-pressure stress space. Thorough evaluation of the new design is conducted via laboratory measurements and finite element simulations. Practical issues and the need for care in specimen preparation and data reduction are explained and discussed. The main motivation behind developing this setup is to aid in characterizing the influence of pressure or negative dilatation on the constitutive shear response of elastomeric coating materials in general and polyurea in particular. Experimental results obtained with the new design illustrate the significant increase in the shear stiffness of polyurea under moderate to high hydrostatic pressures.     

Extremal nozzle contours for gas flows with particle lag

The determination of the extremal nozzle contour for gas flow without foreign particles has been carried out in several studies [1–6], based on the calculation of the flow field using the method of characteristics.In [7, 8] the equations are derived for the characteristics and the relations along the streamlines which are required for calculating two-dimensional gas flow with foreign particles. The variational problem for two-phase flow in the two-dimensional formulation may be solved by the method of Guderley and Armitage [9] with the use of equations given in [7] or [8]; however this method is very tedious, even with the use of high-speed computers.In [10, 11] studies are made of two-phase one-dimensional flows by expanding the unknown functions in series in a small parameter, defined by the particle dimensions. In [12] a solution is given for the variational problem (in the one-dimensional formulation) of designing the contour of a nozzle with maximal impulse. However that study does not take account of the static term appearing in the impulse and the solution is obtained in relative cumbersome form. Moreover, the question of account for the losses due to nonparallelism and nonuniformity of the discharge was not considered.The present paper considers in the one-dimensional formulation the flow of a two-phase medium in a Laval nozzle with small particle lags (in velocity and temperature). The variational problem of determining the maximal nozzle impulse is formulated along the nozzle contour for fixed geometric expansion ratio. The impulse losses due to nonparallelism of the discharge are simulated by a function which depends on the ordinates which are variable along the contour and on the slope of the tangent to the contour.The author wishes to thank Yu. D. Shmyglevskii and A. N. Kraiko for helpful discussions and V. K. Starkov for carrying out the calculations on the computer.     

Stability of elastic bodies under omnilateral compression

Conclusions We have analyzed here the stability of the equilibrium of a simply connected isotropic compressible body with the elastic potential of arbitrary form and under uniform omnilateral deformation. A survey has been given here of earlier results obtained by other authors. The basic celations have been stated in a general form covering the theory of finite subcritical strains and two variants of the theory of small subcritical strains. For the latter theory new relations have been rigorously derived from which perturbations of tracking surface loads can be calculated, on the basis of corresponding expressions in the theory of finite subcritical strains. It has been proven that the sufficient conditions for the applicability of the static method of analysis are satisfied when the same boundary conditions are given over the entire body surface, as well as in several cases of different boundary conditions given at different segments of the boundary surface. It has been shown in a general form, for the theory of finite subcritical strains and for two variants of the theory of small subcritical strains, that the equilibrium of an elastic body under omnilateral deformation is stable, if a tracking load, is given over the entire boundary surface. As an example of problems with different boundary conditions at different segments of the boundary surface, we have considered the conventional problem concerning the stability of a bar on hinge supports and under uniform omnilateral deformation. It has been rigorously proven that in this case the equilibrium is stable when tracking loads are given at the lateral surfaces and is unstable when dead loads are given at the lateral surfaces. These conclusions apply to the theory of finite subcritical strains as well as to the theory of small subcritical strains, and they represent the complete version pertaining to compressible bodies.Institute of Mechanics, Academy of Sciences of the Ukrainian SSR, Kiev. Translated from Prikladnaya Mekhanika, Vol. 12, No. 6, pp. 3–27, June, 1976.     

Analysis of turbulent boundary layer interaction with an external supersonic flow behind a step

An integral method of analyzing turbulent flow behind plane and axisymmetric steps is proposed, which will permit calculation of the pressure distribution, the displacement thickness, the momentum-loss thickness, and the friction in the zone of boundary layer interaction with an external ideal flow. The characteristics of an incompressible turbulent equilibrium boundary layer are used to analyze the flow behind the step, and the parameters of the compressible boundary layer flow are connected with the parameters of the incompressible boundary layer flow by using the Cowles-Crocco transformation.A large number of theoretical and experimental papers devoted to this topic can be mentioned. Let us consider just two [1, 2], which are similar to the method proposed herein, wherein the parameter distribution of the flow of a plane nearby turbulent wake is analyzed. The flow behind the body in these papers is separated into a zone of isobaric flow and a zone of boundary layer interaction with an external ideal flow. The jet boundary layer in the interaction zone is analyzed by the method of integral relations.The flow behind plane and axisymmetric steps is analyzed on the basis of a scheme of boundary layer interaction with an external ideal supersonic stream. The results of the analysis by the method proposed are compared with known experimental data.Notation x, y longitudinal and transverse coordinates - X, Y transformed longitudinal and transverse coordinates - , ^*, ^** boundary layer thickness, displacement thickness, momentum-loss thickness of a boundary layer - , ^*, ^** layer thickness, displacement thickness, momentum-loss thickness of an incompressible boundary layer - u, velocity and density of a compressible boundary layer - U, velocity and density of the incompressible boundary layer - , stream function of the compressible and incompressible boundary layers - , dynamic coefficient of viscosity of the compressible and incompressible boundary layers - r₁ radius of the base part of an axisymmetric body - r radius - R transformed radius - M Mach number - friction stress - p pressure - a speed of sound - s enthalpy - v Prandtl-Mayer angle - P Prandtl number - P_t turbulent Prandtl number - r₂ radius of the base sting - b step depth - =0 for plane flow - =1 for axisymmetric flow Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 33–40, May–June, 1971.In conclusion, the authors are grateful to M. Ya. Yudelovich and E. N. Bondarev for useful comments and discussions.