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1.
Fully developed turbulent pipe flow of an aqueous solution of a rigid “rod-like” polymer, scleroglucan, at concentrations of 0.005% (w/w) and 0.01% (w/w) has been investigated experimentally. Fanning friction factors were determined from pressure-drop measurements for the Newtonian solvent (water) and the polymer solutions and so levels of drag reduction for the latter. Mean axial velocity u and complete Reynolds normal stress data, i.e. u′, v′ and w′, were measured by means of a laser Doppler anemometer at three different Reynolds numbers for each fluid. The measurements indicate that the effectiveness of scleroglucan as a drag-reducing agent is only mildly dependent on Reynolds number. The turbulence structure essentially resembles that of flexible polymer solutions which also lead to low levels of drag reduction.  相似文献   

2.
A turbine blade is modelled as a uniform isotropic prismatic beam of general cross-section and “setting angle” rotating about one end, and is analysed according to the linear theory of elasticity. A semi-inverse solution is presented which reduces the three-dimensional problem to one of two dimensions, and explicit stress and strain components given for the mathematically amenable elliptic cross-section. As expected, the planar stresses σx,σy, and τxy arising from the two-dimensional problem are found to be small. For the general section, the theory predicts small curvature of the blade centre line, and a twisting moment which tends to reduce the “angle of set”.  相似文献   

3.
The strain energy density theory is applied to analyze the fracture instability of a mechanical system whose behavior is governed by the interaction of geometry, load and material inhomogeneity. This is accomplished by obtaining the location of the global and local relative minima of the strain energy density function dW/dV denoted, respectively, by [(dW/dV)min]g and [(dW/dV)min]¢l. The former refers to a fixed global coordinate system for the entire solid while the latter corresponds to local coordinate systems referred to each material point. An unique length parameter “ℓ” representing the distance between [(dW/dV)minmax]g and [(dW/dV)minmax] can thus be found and serves as a measure of the degree of system instability tending toward failure by fracture.Numerical results are obtained and displayed graphically for the case of a solid containing an inclusion of dissimilar material. The changes that take place in material inhomogeneity, loading type and physical dimensions of the solid and inclusion are reflected through ℓ. The method suggests the compatibility of ℓ for each member of a multi-component structure in order to avoid premature failure of a single member.  相似文献   

4.
The dynamic behavior of vehicles which are equipped with pneumatic tires depends, to a degree, on the properties of the tire. Therefore, road handling and comfort are also affected by tire characteristics. When the inflation pressure is reduced one obtains a softer “spring”. The dynamic spring coefficient Cdyn increases with increasing rolling speed. Damping coefficient k is related to the excitation frequency by a power function. This function shows a sharp negative slope for low velocities. These conclusions apply to the tire types and test conditions described in this paper.  相似文献   

5.
The derivation of the overall behaviour of nonlinear viscoelastic (or rate-dependent elastoplastic) heterogeneous materials requires a linearisation of the constitutive equations around uniform per phase stress (or strain) histories. The resulting Linear Comparison Material (LCM) has to be linear thermoviscoelastic to fully retain the viscoelastic nature of phase interactions. Instead of the exact treatment of this LCM (i.e., correspondence principle and inverse Laplace transforms) as proposed by the “classical” affine formulation, an approximate treatment is proposed here. First considering Maxwellian behaviour, comparisons for a single phase as well as for two-phase materials (with “parallel” and disordered morphologies) show that the “direct inversion method” of Laplace transforms, initially proposed by Schapery (1962), has to be adapted to fit correctly exact responses to creep loading while a more general method is proposed for other loading paths. When applied to nonlinear viscoelastic heterogeneous materials, this approximate inversion method gives rise to a new formulation which is consistent with the classical affine one for the steady-state regimes. In the transient regime, it leads to a significantly more efficient numerical resolution, the LCM associated to the step by step procedure being no more thermoviscoelastic but thermoelastic. Various comparisons for nonlinear viscoelastic polycrystals responses to creep as well as relaxation loadings show that this “quasi-elastic” formulation yields results very close to classical affine ones, even for high contrasts.  相似文献   

6.
These experiments, involving the transverse oscillations of an elastically mounted rigid cylinder at very low mass and damping, have shown that there exist two distinct types of response in such systems, depending on whether one has a low combined mass-damping parameter (low m*ζ), or a high mass-damping (highm*ζ ). For our low m*ζ, we find three modes of response, which are denoted as an initial amplitude branch, an upper branch and a lower branch. For the classical Feng-type response, at highm*ζ , there exist only two response branches, namely the initial and lower branches. The peak amplitude of these vibrating systems is principally dependent on the mass-damping (m*ζ), whereas the regime of synchronization (measured by the range of velocity U*) is dependent primarily on the mass ratio, m*ζ. At low (m*ζ), the transition between initial and upper response branches involves a hysteresis, which contrasts with the intermittent switching of modes found, using the Hilbert transform, for the transition between upper–lower branches. A 180° jump in phase angle φ is found only when the flow jumps between the upper–lower branches of response. The good collapse of peak-amplitude data, over a wide range of mass ratios (m*=1–20), when plotted against (m*+CA) ζ in the “Griffin” plot, demonstrates that the use of a combined parameter is valid down to at least (m*+CA)ζ 0·006. This is two orders of magnitude below the “limit” that had previously been stipulated in the literature, (m*+CA) ζ>0·4. Using the actual oscillating frequency (f) rather than the still-water natural frequency (fN), to form a normalized velocity (U*/f*), also called “true” reduced velocity in recent studies, we find an excellent collapse of data for a set of response amplitude plots, over a wide range of mass ratiosm* . Such a collapse of response plots cannot be predicted a priori, and appears to be the first time such a collapse of data sets has been made in free vibration. The response branches match very well the Williamson–Roshko (Williamson & Roshko 1988) map of vortex wake patterns from forced vibration studies. Visualization of the modes indicates that the initial branch is associated with the 2S mode of vortex formation, while the Lower branch corresponds with the 2P mode. Simultaneous measurements of lift and drag have been made with the displacement, and show a large amplification of maximum, mean and fluctuating forces on the body, which is not unexpected. It is possible to simply estimate the lift force and phase using the displacement amplitude and frequency. This approach is reasonable only for very low m*.  相似文献   

7.
As is shown in the first paper of the series, the main factor responsible for concentrated (‘neck-like’) deformation in high-speed melt spinning is the gradient of elongational viscosity along the spinline. In the present paper, stress-induced polymer crystallization is analyzed as a potential source of the rapid viscosity increase.A model of crystallization-controlled solidification is proposed, in which viscosity of the polymer increases with the degree of crystallinity, Θ, as
, reaching infinity (complete solidification) at Θ = Θcr. The critical crystallinity level has been interpreted as one required for ‘crosslinking’ of polymer chains present in the melt.In addition to viscosity increase, crystallization modifies the local temperature in the spinline and reduces viscosity.The analysis of stress effects shows that critical crystallization temperature, Tm, and crystallization rate, K, increase with the square of normal stress difference in the spinline, Δp = pxxprr. The onset of crystallization can be shifted by 20–40 K towards higher temperatures, and crystallization rate can increase by orders of magnitude when high take-up speeds increase the stress level.A simple model illustrating velocity profiles in crystallizing Newtonian jets is discussed.The analysis strongly supports the hypothesis that the high viscosity gradient resulting from rapid stress-induced crystallization provides the major mechanism of ‘neck-like’ deformation.  相似文献   

8.
The objective of the present Note is to estimate the equivalent torsion rigidity modulus for a cylinder whose cross-section Σ exhibits a periodical distribution of porous zones ΣP. Taking into account a second, finer, periodical distribution of pores in ΣP, we have to use the homogenization method in a biperiodical context. However, the contrast of scales at the interfaces between ΣP and the compact part ΣC of Σ, requires some subtle fitting up of this method. Finally, we point out the existence of boundary layers around the interfaces ∂ΣP and we estimate the weakening of the torque rigidness. To cite this article: M'B. Taghite et al., C. R. Mecanique 334 (2006).  相似文献   

9.
Using the technique of Dimensional Analysis the phenomenon of crack closure is modelled using the concept of a contact stress intensity factor Kc. For constant amplitude loading, a simple expression, Kcmax = g(R) ΔK, is obtained without making idealized assumptions concerning crack tip behaviour. Further, by assuming that crack closure arises from the interaction of residual plasticity in the wake of the crack and crack tip compressive stresses, the function g(R) is shown to be constant for non-workhardening materials. This implies that any dependency of Kcmax on R must be attributed to the workhardening characteristic of the material. With Kc known, an “effective” stress intensity factor Ke may be calculated and incorporated into a crack growth law of the form da/dn = f(ΔKe). From analysis, it can be deduced that for a workhardening material, Kcmax will decrease as R increases and the effective stress intensity factor will increase. This means that the fatigue crack propagation rate will increase with R, in accordance with experimental observations.  相似文献   

10.
The Volterra-Wiener functional expansion is employed to the analysis of statistic properties for random heterogeneous solids. For simplicity, the technique is displayed on an elastic suspension of spheres. The basis function in the expansion is chosen as that corresponding to the so-called “perfect disorder” of spheres (PDS), recently introduced by the authors. An infinite hierarchy of equations for the kernels in the expansion is derived whose truncating after the nth equation is shown to yield results for the averaged statistical characteristics which are valid to order cnf, where cf is the volume fraction of the spheres. The kernels for the first and the second approximations, n = 1, 2, are found and related to the displacement fields in an infinite elastic body containing, respectively, one and two spherical inhomogeneities. Within the frame of the so-called singular approximation the overall tensor of elastic moduli for a suspension of perfectly disordered spheres is shown to coincide to the order c2f with a formula, earlier obtained by means of the method of the effective field.  相似文献   

11.
The implicit character of micro-structural degradation is determined by specifying the time history of crack growth caused by creep–fatigue interaction at high temperature. A dual scale micro/macro-equivalent crack growth model is used to illustrate the underlying principle of multiscaling which can be applied equally well to nano/micro. A series of dual scale models can be connected to formulate triple or quadruple scale models. Temperature and time-dependent thermo-mechanical material properties are developed to dictate the design time history of creep–fatigue cracking that can serve as the master curve for health monitoring.In contrast to the conventional procedure of problem/solution approach by specifying the time- and temperature-dependent material properties as a priori, the desired solution is then defined for a class of anticipated loadings. A scheme for matching the loading history with the damage evolution is then obtained. The results depend on the initial crack size and the extent of creep in proportion to fatigue damage. The path dependent nature of damage is demonstrated by showing the range of the pertinent parameters that control the final destruction of the material. A possible scenario of 20 yr of life span for the 38Cr2Mo2VA ultra-high strength steel is used to develop the evolution of the micro-structural degradation. Three micro/macro-parameters μ*, d* and σ* are used to exhibit the time-dependent variation of the material, geometry and load effects. They are necessary to reflect the scale transitory behavior of creep–fatigue damage. Once the algorithm is developed, the material can be tailor made to match the behavior. That is a different life span of the same material would alter the time behavior of μ*, d* and σ* and hence the micro-structural degradation history. The one-to-one correspondence of the material micro-structure degradation history with that of damage by cracking is the essence of path dependency. Numerical results and graphs are obtained to demonstrate how the inherently implicit material micro-structure parameters can be evaluated from the uniaxial bulk material properties at the macroscopic scale.The combined behavior of creep and fatigue can be exhibited by specifying the parameter ξ with reference to the initial defect size a0. Large ξ (0.90 and 0.85) gives critical crack size acr = 11–14 mm (at t < 20 yr) for a0 about 1.3 mm. For small ξ (0.05 and 0.15), there results critical acr = 6–7 mm (at t < 20 yr) for a0 about 0.7–0.8 mm. The initial crack is estimated to increase its length by an order of magnitude before triggering global to the instability. This also applies ξ ≈ 0.5 where creep interacts severely with fatigue. Fine tuning of acr and a0 can be made to meet the condition oft = 20 yr.Trade off among load, material and geometric parameters are quantified such that the optimum conditions can be determined for the desired life qualified by the initial–final defect sizes. The scenario assumed in this work is indicative of the capability of the methodology. The initial–final defect sizes can be varied by re-designing the time–temperature material specifications. To reiterate, the uniqueness of solution requires the end result to match with the initial conditions for a given problem. This basic requirement has been accomplished by the dual scale micro/macro-crack growth model for creep and fatigue.  相似文献   

12.
The motivation to examine physical events at even smaller size scale arises from the development of use-specific materials where information transfer from one micro- or macro-element to another could be pre-assigned. There is the growing belief that the cumulated macroscopic experiences could be related to those at the lower size scales. Otherwise, there serves little purpose to examine material behavior at the different scale levels. Size scale, however, is intimately associated with time, not to mention temperature. As the size and time scales are shifted, different physical events may be identified. Dislocations with the movements of atoms, shear and rotation of clusters of molecules with inhomogeneity of polycrystals; and yielding/fracture with bulk properties of continuum specimens. Piecemeal results at the different scale levels are vulnerable to the possibility that they may be incompatible. The attention should therefore be focused on a single formulation that has the characteristics of multiscaling in size and time. The fact that the task may be overwhelmingly difficult cannot be used as an excuse for ignoring the fundamental aspects of the problem.Local nonlinearity is smeared into a small zone ahead of the crack. A “restrain stress” is introduced to also account for cracking at the meso-scale.The major emphasis is placed on developing a model that could exhibit the evolution characteristics of change in cracking behavior due to size and speed. Material inhomogeneity is assumed to favor self-similar crack growth although this may not always be the case. For relatively high restrain stress, the possible nucleation of micro-, meso- and macro-crack can be distinguished near the crack tip region. This distinction quickly disappears after a small distance after which scaling is no longer possible. This character prevails for Mode I and II cracking at different speeds. Special efforts are made to confine discussions within the framework of assumed conditions. To be kept in mind are the words of Isaac Newton in the Fourth Regula Philosophandi:
Men are often led into error by the love of simplicity which disposes us to reduce things to few principles, and to conceive a greater simplicity in nature than there really isWe may learn something of the way in which nature operates from fact and observation; but if we conclude that it operates in such a manner, only because to our understanding that operates to be the best and simplest manner, we shall always go wrong.”––Isaac Newton

Article Outline

1. Introduction
2. Elastodynamic equations and moving coordinates
3. Moving crack with restrain stress zone
3.1. Mode I crack
3.2. Mode II crack
4. Strain energy density function
4.1. Mode I
4.2. Mode II
5. Conclusions
Acknowledgements
References

1. Introduction

Even though experimental observations could reveal atomic scale events, in principle, analytical predictions of atomic movements fall short of expectation by a wide margin. Classical dislocation models have shown to be inadequate by large scale computational schemes such as embedded atoms and molecular dynamics. Lacking in particular is a connection between interatomic (10−8 cm) processes and behavior on mesoscopic scale (10−4 cm) [1]. Relating microstructure entities to macroscopic properties may represent too wide of a gap. A finer scale range may be needed to understand the underlying physics. Segmentation in terms of lineal dimensions of 10−6–10−5, 10−5–10−3 and 10−3–10−2 cm may be required. They are referred to, respectively, as the micro-, meso- and macro-scale. Even though the atomistic simulation approach has gained wide acceptance in recent times, continuum mechanics remains as a power tool for modeling material behavior. Validity of the discrete and continuum approach at the different length scales has been discussed in [2 and 3].Material microstructure inhomogeneities such as lattice configurations, phase topologies, grain sizes, etc. suggest an uneven distribution of stored energy per unit volume. The size of the unit volume could be selected arbitrarily such as micro-, meso- or macroscopic. When the localized energy concentration level overcomes the microstructure integrity, a change of microstructure morphology could take place. This can be accompanied by a corresponding redistribution of the energy in the system. A unique correspondence between the material microstructure and energy density function is thus assumed [4]. Effects of material structure can be reflected by continuum mechanics in the constitutive relations as in [5 and 6] for piezoelectric materials.In what follows, the energy density packed in a narrow region of prospective crack nucleation sites, the width of this region will be used as a characteristic length parameter for analyzing the behavior of moving cracks in materials at the atomic, micro-, meso- and macroscopic scale level. Nonlinearity is confined to a zone local to the crack tip. The degree of nonlinearity can be adjusted by using two parameters (σ0,ℓ) or (τ0,ℓ) where σ0 and τ0 are referred to, respectively, as the stresses of “restraint” owing to the normal and shear action over a local zone of length ℓ. The physical interpretation of σ0 and τ0 should be distinguished from the “cohesive stress” and “yield stress” initiated by Barenblatt and Dugdale although the mathematics may be similar. The former has been regarded as intrinsic to the material microstructure (or interatomic force) while the latter is triggered by macroscopic external loading. Strictly speaking, they are both affected by the material microstructure and loading. The difference is that their pre-dominance occurs at different scale levels. Henceforth, the term restrain stress will be adopted. For simplicity, the stresses σ0 and τ0 will be taken as constants over the segment ℓ and they apply to the meso-scale range as well.

2. Elastodynamic equations and moving coordinates

Navier’s equation of motion is given by(1)in which u and f are displacement and body force vector, respectively. Let the body force equal to zero, and introduce dilatational displacement potential φ(x,y,t) and the distortional displacement potential ψ(x,y,t) such that(2)u=φ+×ψThis yields two wave equations as(3)where 2 is the Laplacian in x and y while dot represents time differentiation. The dilatational and shear wave speeds are denoted by cd and cs, respectively.For a system of coordinates moving with velocity v in the x-direction,(4)ξ=xvt, η=ythe potential function φ(x,y,t) and ψ(x,y,t) can be simplified to(5)φ=φ(ξ,η), ψ=ψ(ξ,η)Eq. (3) can thus be rewritten as(6)in which(7)In view of Eqs. (7), φ and ψ would depend on (ξ,η) as(8)φ(ξ,η)=Re[Fd)], ψ(ξ,η)=Im[Gs)]The arguments ζj(j=d,s) are complex:(9)ζj=ξ+iαjη for j=d,sThe stress and displacement components in terms of φ and ψ are given as(10)uy(ξ,η)=−Im[αdFd)+Gs)]The stresses are(11)σxy(ξ,η)=−μ Im[2αdFd)+(1+αs2)Gs)]σxx(ξ,η)=μ Re[(1−αs2+2αd2)Fd)+2αsGs)]σyy(ξ,η)=−μ Re[(1+αs2)Fd)+2αsGs)]with μ being the shear modulus of elasticity.

3. Moving crack with restrain stress zone

The local stress zone is introduced to represent nonlinearity; it can be normal or shear depending on whether the crack is under Mode I or Mode II loading. For Mode I, a uniform stress σ is applied at infinity while τ is for Mode II. The corresponding stress in the local zone of length ℓ are σ0 are τ0. They are shown in Fig. 1 for Mode I and Fig. 2 for Mode II. Assumed are the conditions in the Yoffé crack model. What occurs as positive at the leading crack edge, the negative is assumed to prevail at the trailing edge.  相似文献   

13.
The rheological properties of dense suspensions, of silica, iron (III) oxide and water, were studied over a range of solids concentrations using a viscometer, which was modified so as to prevent settling of the solid components. Over the conditions studied, the material behaved according to power—law flow relationships. As the concentrations of silica and iron(III) oxide were increased, an entropy term in the flow equation was identified which had a silica dependent and an iron (III) oxide dependent component. This was attributed to a tendency to order into some form of structural regularity. A, A, B, C pre-exponential functions (K Pan s–1) - C ox volume fraction iron (III) oxide - Q activation energy (kJ mol–1) - R gas constant (kJ mol–1 K–1) - R v silica/water volume ratio - T temperature (K) - n power-law index - H enthalpy (kJ mol–1) - S entropy change (kJ mol–1 K–1) - shear strain rate (s–1) - shear stress (Pa)  相似文献   

14.
Finite-volume, semi-elliptic computations are reported of the three-dimensional flow around a 90° square-sectioned bend for which detailed laser-Doppler measurements have been reported by Taylor et al.1 While the standard k- eddy-viscosity model has been used in the main flow region, in place of the usual “wall functiond”, the mixing-length hypothesis has been employed to resolve the flow in the layer immediately adjacent to the wall. The scheme is successful in predicting the details of the primary and secondary flow fields both within the bend and downstream thereof.  相似文献   

15.
16.
The fatigue crack growth characteristics of CrlMo steel have been investigated at 861 K over the R-ratio range 0.1–0.7 utilising a dwell time of 10 min. at maximum load. All tests were conducted under load control in a laboratory air environment. It was established that the R-ratio significantly affected the fatigue crack extension behaviour inasmuch that with increasing R-ratio, the critical ΔK level for the onset of creep fatigue interactive growth, ΔKIG, decreased from 20 to 7 MPa√m and the threshold stress intensity, ΔKth, decreased from 9 to about 3 MPa√m. At intermediate ΔK levels, i.e. between ΔKth and ΔKIG, the fatigue crack extension rates, for all R-ratio values, resided on or slightly below the CTOD line, which represents the upper bound for contrnuum controlled fatigue crack growth. Creep fatigue interactive growth was typified by crack extension rates that reside above the CTOD line with a ΔKIG dependence; the attainment of some critical creep condition or crack linkage condition which causes the abrupt change in crack extension behaviour at ΔKIG; and crack extension occurs almost exclusively in an intergranular manner. The R-ratio and ΔKIG followed a linear relation. A literature review concerning the effect of temperature on the threshold fatigue crack growth characteristics of low alloy ferritic steels demonstrated powerful effects of temperature; the magnitude of these effects, however, were dependent upon the testing temperature regime and R-ratio level. The effect of R-ratio on ΔKth was greatest at temperatures >400°C, significant at ambient temperatures and least in the temperature range 90°C to <300°C. The relationship between temperature and ΔKth, at a given R-ratio, exhibited a through and a minimum ΔKth value was observed in the temperature range 200–250°C. The magnitude of the temperature effects on ΔKth decreased with increasing R-ratio. Such effects of temperature and R-ratio on ΔKth was reasonably explained in terms of crack closure effects. Finally, the present elevated temperature fatigue crack growth data exhibited massive crack extension enhancement values when compared to ambient near-threshold fatigue crack growth data for CrlMo steel. Such large enhancement values were the combined effects of temperature (environment) and frequency.  相似文献   

17.
Examined experimentally are the influence of stress triaxiality and temperature on the growth of microvoids and the ductile/brittle transition (DBT) macrobehavior of 40 Cr steel subjected to two different heat treatments. This is accomplished by testing more than 300 smooth and notched specimens over a temperature range of 20°C to −196°C. Changes in the microstructure morphology are examined by scanning electron microscopy (SEM) and identified with fracture data on a surface constructed from the uniaxial strain εc at fracture, the stress triaxiality Rσ and the temperature T. While stress triaxiality has a significant influence on the DBT temperature Tc, it does not affect the ratio of the average radius of voids Ro to that of inclusions Ri. The ratio Ro/Ri is found to increase with temperature and remains constant in specimens with different notch radii regardless of the temperature. Empirical relations between Tc and Rσ and Ro/Ri and T are proposed to better understand how macrofracture parameters are influenced by microstructure entities.  相似文献   

18.
The effects of physical aging on fracture and yielding behavior are polycarbonate are considered. Two groups of Bisphenol A-based polycarbonate, consisted of extruded PC sheets (thickness of 0.25 mm) and injection molded PC bars (thickness of 3.18 mm) are used. These samples were annealed at various temperatures ranging from 60 to 120 °C, for different times varying up to 240 h. For PC sheets the essential work of fracture (EWF) method was used to analyze fracture behavior. The results are compared to the strain energy density with aging time and aging temperature in the ranges investigated. This effect is confirmed by the change in fracture toughness, as measured by three-point bending tests. The concept of fictive temperature (Tf) was used to characterize the degree of aging in the sample. Tf of a glass in an aged state at a time t is defined as the temperature at which the volume would be equal to the equilibrium volume at Tf if the sample were instantaneously removed to that temperature. Differential scanning calorimetry (DSC) was used to determine Tf. The variations of Tf with aging time and aging temperature are in agreement with both the strain energy density measurement and the three-point bending tests. These results contradict the effects of aging on fracture toughness observed by the essential work of fracture approach. The latter showed anomalous regions of increasing fracture toughness with aging, leading to spurious conclusions. The brittle–ductile transition in fracture behavior is analyzed by an activation energy approach. Aging increases the brittle–ductile transition temperature and the effect is more pronounced for the lower molecular-weight sample. Fracture tests also showed a decrease in the entropy with aging, confirming the results observed previously from tension and compression tests.  相似文献   

19.
Experimental observations suggest that for perfectly-plastic materials containing pores, the (small) strain at which significant macroscopic yielding occurs is relatively insensitive to porosity, for volume fractions below approximately 15–20% (although the yield stress drops significantly with increasing porosity). Another observation is that, at these porosity levels, the stress–strain curve remains approximately linear almost up to the yield point. Based on these observations, Sevostianov and Kachanov constructed yield surfaces that explicitly reflect the shapes of the pores and their orientation. The underlying microscale mechanism is that local plastic “pockets” near pores blunt the stress concentrations; as a result, they remain limited in size and well contained in the elastic field until they connect and almost the entire matrix plasticizes within a narrow interval of stresses that can be idealized as the yield point. The present paper provides direct insight into the micromechanics of poroplasticity through direct microscale numerical simulation. Besides confirming the basic microscale mechanism, these simulations reveal that the reduction of the macroscopic poroplastic yield stress is approximated quite closely by 1−v2 times the dense nonporous yield stress, where v2 is the volume fraction of the pores.  相似文献   

20.
Mechanisms of brittle-ductile transition in toughened thermoplastics   总被引:1,自引:0,他引:1  
The objective of this work was to investigate the mechanism of brittle-ductile transition in toughened polymers. Two systems, namely, a rubber-toughened nylon 66 (Zytel ST-801) and a high impact polystyrene (HIPS), were chosen for this study. The samples were prepared by injection molding and were tested in three-point bending under various loading rates and temperatures. The brittle-ductile transition temperature (Tb–d) was determined from the observed fracture behavior as a function of temperature. Molecular relaxation temperatures of the polymers were measured by mechanical spectroscopy at various frequencies. The correlation between temperature and loading rate was estimated using the Arrhenius equation. The results show that Tb–d of Zytel ST-801 is only slightly affected by the loading rate, whereas Tb–d of HIPS strongly increases with deformation rate. It is found that for the former, within the experimental errors, an increase in Tb–d with loading rate corresponds to the shift in the secondary relaxation temperature Tb of the nylon 66 matrix. For the latter however, the increase in Tb–d is related to the glass/rubber relaxation of the polystyrene matrix. It seems that the type of molecular relaxation controlling the brittle-ductile transition corresponds to that with lower activation energy.  相似文献   

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