Technical Brief. Journal of Biomechanical Engineering. Christof Hurschler 1. Paolo P. Provenzano. Ray Vanderby, Jr. 2.

Size: px
Start display at page:

Download "Technical Brief. Journal of Biomechanical Engineering. Christof Hurschler 1. Paolo P. Provenzano. Ray Vanderby, Jr. 2."

Transcription

1 Journal of Biomechanical Engineering Technical Brief Application of a Probabilistic Microstructural Model to Determine Reference Length and Toe-to- Linear Region Transition in Fibrous Connective Tissue Christof Hurschler 1 Paolo P. Provenzano Ray Vanderby, Jr. 2 Department of Orthopedics and Rehabilitation and Department of Biomedical Engineering, University of Wisconsin, Madison, WI This study shows how a probabilistic microstructural model for fibrous connective tissue behavior can be used to objectively describe soft tissue low-load behavior. More specifically, methods to determine tissue reference length and the transition from the strain-stiffening toe-region to the more linear region of the stress-strain curve of fibrous connective tissues are presented. According to a microstructural model for uniaxially loaded collagenous tissues, increasingly more fibers are recruited and bear load with increased tissue elongation. Fiber recruitment is represented statistically according to a Weibull probability density function (PDF). The Weibull PDF location parameter in this formulation corresponds to the stretch at which the first fibers begin to bear load and provides a convenient method of determining reference length. The toe-to-linear region transition is defined by utilizing the Weibull cumulative distribution function (CDF) which relates the fraction of loaded fibers to the tissue elongation. These techniques are illustrated using representative tendon and ligament data from the literature, and are shown to be applicable retrospectively to data from specimens that are not heavily preloaded. The reference length resulting from this technique provides an objective datum from which to calculate stretch, strain, and tangent modulus, while the Weibull CDF provides an objective parameter with which to characterize the limits of lowload behavior. DOI: / Current address: Orthopadische Klinik, Medizinische Hochschule Hannover, Anna-von-Borries-Str. 1 7, D Hannover, Germany. 2 Ray Vanderby Jr., Orthopedic Research Laboratories, K4/738, 600 Highland Avenue, University of Wisconsin, Madison, Madison, WI vanderby@surgery.wisc.edu. Contributed by the Bioengineering Division for publication in the JOURNAL OF BIOMECHANICAL ENGINEERING. Manuscript received by the Bioengineering Division December 4, 2001; revised manuscript received November 19, Associate Editor: M. S. Sacks. Introduction The first goal of this study is to develop an objective method to define the reference length for soft fibrous connective tissues. Reference length is the basis for biomechanical descriptions, yet it is not selected in a consistent way throughout the literature. Reference length of a tendon or ligament specimen is often determined empirically by increasing deformation until a measurable load is detected, 1,2 a small arbitrarily assigned preload is applied, 3 5 or an inflection is observed in the load-deformation curve, 6,7. Tendon and ligament specimens, however, are compliant at the onset of load bearing such that small changes in load result in relatively large variations in reference length. In addition, relatively large preloads are sometimes applied that mask much of the toe-in region of the load-deformation response. Since stretch-ratio or strain is a normalized quantity, based on the reference length of the specimen, different choices of preload can introduce bias into biomechanical measures such as stretch, strain, strain to failure, or tangent modulus. The second goal of this study is to develop an objective method to identify the transition from the strain-stiffening toe-region to the linear region commonly observed in the stress-strain diagrams of fiber recruiting soft tissues. The definition of such a point will aid the study of low-load behavior in normal and pathologic connective tissues. Constitutive models, 8 14, have been developed using the assumption that the strain stiffening behavior of the toe-region results from gradual recruitment of collagen fibers during tissue elongation, 15, and that the fiber recruitment can be described by a probability density function PDF 8,9,11 13,16. Straightening of collagen fibers after the application of low loads has also been observed using scanning electron microscopy, 17. It should be noted that in this study low-load refers to the stresses present in the toe-region. Once a substantial percentage of fibers are recruited, tissue behavior transitions from the toe-region to a more linear region of the stress-stretch or strain curve. Although, many models fit the nonlinear behavior of fibrous connective tissue very well, the specific transition from the toe-region to the more linear portion of the curve has undergone less scrutiny. Most biomechanical studies of soft tissues, such as ligament and tendon, focus on the middle linear and upper failure portions of the stress-stretch curve, while the equally important lower toe portion of the curve is less described. The ability to characterize the low-load region would increase a researcher s ability to understand and compare tissue behavior and the effect of treatment regimes. Panjabi et al. 18 characterized normal and subfailure damaged rabbit anterior cruciate ligament load-deformation behavior by measuring the tissue deformation at 5, 10, 25, and 50% of the previously determined failure force. Results of their study indicate a change in the load-deformation behavior manifested by significantly larger deformations in the lower half of the load-deformation curve. Nonetheless, more detailed descriptions of these changes in the lower portion of the structural or material property curve are largely unrealized due to the lack of objective parameters by which they can be characterized. Journal of Biomechanical Engineering Copyright 2003 by ASME JUNE 2003, Vol. 125 Õ 415

2 Several structural and microstructural models have been used to study the mechanical properties of various tissues 8,9,11 13,16. Hurschler et al. 11 previously developed a model that assumes increasing collagen fiber straightening and load bearing with increasing elongation i.e., fiber recruitment from a crimped or slack to a load bearing according to a Weibull 19 probability density function. Because it is an asymmetric one-tailed function, a parameter represented by a Weibull PDF has a zero probability of occurrence below a certain value. The Weibull PDF was chosen to represent fiber straightening in ligaments and tendons since in a slack configuration, no fibers have yet straightened to bear loads. Thus, fiber straightening is well represented by the one-tailed nature of the Weibull PDF. In contrast to the Gaussian PDF which is described by two parameters i.e., the mean and the standard deviation, the Weibull distribution is described by three parameters: shape, scale, and location, 20. In the context of the structural model, the shape and scale parameters are related to the shape of the toe-region where the fibers are being recruited; the location parameter is related to the stretch at which the first fibers begin to bear load. This location parameter, described in detail later in this manuscript, provides a parameter to objectively determine reference length of the tissue. An objective reference length provides a consistent basis for describing the material properties in the high load and low load regions of fibrous tissues. Hence, the goals of this study were: 1 to introduce the location parameter as a preload independent parameter to establish a reference length in biomechanical evaluations of fibrous connective tissues, such as ligaments and tendons, and 2 to establish a method for quantifying the toe-to-linear region transition-point in strain-stiffening soft fibrous tissues. In order to examine the first goal, representative data from the literature, 21, are used to illustrate how may be applied to data gathered from either initially slack or preloaded specimens. Also shown is how the experimental choice of reference length affects tangent modulus. In order to examine the second goal, the model is applied to previously published data for normal and damaged tissue, 22, to illustrate how it can be used to quantify microstructural changes which occur in the altered toe-to-linear region transition. Methods Microstructural Model. The probabilistic microstructural model 3 applied in this study is described in detail by Hurschler et al. 11 and will therefore only be briefly described here. The unloaded tissue is assumed to be dominantly composed of crimped collagen fibers that need to be extended various lengths before they begin to bear tensile load. Fibers are assumed to be oriented predominately along the longitudinal axis of the ligament or tendon. The straightening stretch ratio SRR, defined as the tissue stretch at which an individual fiber begins to bear load, is described as s l s /l o fiber length divided by tissue reference length. The load borne by the fiber is assumed to behave according to a constitutive law based on collagen fibril microstructure. The stress in the tissue is determined by the overall tissue stretch stretch ratio t l/l 0 deformed tissue length divided by tissue reference length and the deformation state, and hence load bearing contribution, of the fiber population. Thus, the longitudinal normal tissue stress ( t ) can be computed by integrating the contribution of all fibers over all possible SSRs ( s ): t t tpw s 33 t / s d s, t. (1) In Eq. 1, P w is the Weibull PDF as a function of SSR, 33 is the longitudinal normal stress in a fiber, and is the location parameter of the Weibull distribution and defines the onset of fiber loading. Hence, t ( t )0 when t, since none of the fibers are 3 The model by Hurschler et al. 11 has been implemented in Microsoft Excel and is available upon request. Please contact the corresponding author to obtain a copy of the model for research and academic purposes. loaded below the threshold. It should be noted however, that can be less than or greater than one depending on whether the tissue is initially in a preloaded or slack configuration, respectively. The form of the Weibull PDF used in Eq. 1 is P w s s 1 exp s, s P w s 0, s. (2) In Eq. 2, is the location parameter as stated above, and and are the shape and scale parameters, respectively. The shape, scale, and location parameters must all be greater than zero i.e., 0, 0, and 0 since stretch ratio is defined to be greater than zero. Shape and scale parameters are related to the shape of the toe-region while the location parameter is related to the stretch at which fibers begin to bear load. The Weibull PDF parameters,, and for a given set of stress-stretch data are determined by a nonlinear least-squares minimization, 11. Determining Tissue Reference Length. Consider a segment uniaxially loaded fibrous tissue such as tendon or ligament consisting of a population of collagen fibers. We define the true axial reference length l 0 of this segment of tissue as the length at which the first fibers straighten and just begin to bear load. Since the fibers comprising the tissue generally do not all straighten at once with elongation, there is in general no sharp discontinuity of the load-displacement curve signaling the attainment of l 0. The distance between the endpoints of the specimen determines the length l of the segment, which in an arbitrary state of deformation may be greater than, or less than, or equal to l 0. Let l r represent the experimentally assigned reference length based on specimen preload upon which measurement of stretch or strain are typically based. Then, generally, l r l 0, in which case the specimen is under some preload. If, on the other hand, l r l 0, the specimen is slack at that reference length and bears no load. Tissue stretch-ratio defined in terms of l 0 is t l/l 0. Stretchratio with respect to l r is primed, t l/l r. The stretch-ratio defined with respect to l r at which fibers just begin to bear load is t0 l 0 /l r. When t0 is known, stretch-ratio relative to l 0 can be obtained by t l l l r t l 0 l r l 0 t0. (3) Thus, if t0 is known, it is possible to convert from stretch based on an arbitrarily assigned reference length l r to stretch based on l 0. A technique by which t0, and hence l 0, can be determined independent of arbitrary load thresholds is now described. As stated in the previous subsection, the Weibull shape and scale parameters and determine the shape of the PDF for fiber straightening stretch and hence the shape of the toe-in region. Within the assumptions of the model, the location parameter determines the stretch at which fibers are first recruited and bear load by definition of the Weibull PDF, the probability that s is zero. Since, by definition, the stretch at which fibers first bear load being t0 l 0 /l r, thus t0. By fitting the model to the experimental stress-stretch data based on l r, t0, and it is possible to compute the stretch-ratio based on l 0 using Eq. 3 from stretch normalized with respect to the experimental reference length l r. It is important to note that the location parameter and hence t0 ) may take values greater or less than one. Thus, if 1 the specimen was initially slack before any load was applied, if 1 the specimen was initially preloaded which is the prevailing experimental practice. Typically, stress is zeroed at the preloaded reference length; in such cases it is still possible to determine the stress offset ( 0 ) associated with the specimen preload by evaluating Eq. 1 at t 1. This stress offset is automatically incorporated into the least-squares algorithm when becomes less than one and adds no additional parameters to the minimization. 416 Õ Vol. 125, JUNE 2003 Transactions of the ASME

3 Fig. 1 Example tendon stress-stretch data taken from Abrahams 21, retaining the units of the original paper. The open symbols represent data points, the dashed line represents the fit of the model to the data. Thus, by obtaining the Weibull PDF parameters from the experimental data based on l r, it is possible to adjust the stress-stretch data to include the stress offset ( 0 ) from the objective reference length l 0. As an example application, the proposed technique of determining t0 is applied to representative tendon data from the literature, 21, retaining the units used in the original paper. The original data ( t ) refers to stress and stretch based reference length l r, determined by some arbitrary preload, and adjusted data ( t ) refers to stress and stretch based on t0 determined by the model Eqs. 1 and 3. For purposes of illustration of the technique, load versus length data is computed by assuming an original specimen gauge length l r of 10 length units Fig. 1. Fitting the model to the original data results in t which indicates that a very small preload was applied to the specimen since 1) and that the chosen reference length for this specimen was Fig. 2 Simulated initially slack tendon stress-stretch data for a reference length of l r Ä9.9 length units open circles. Adjusted stress-stretch data and corresponding model fit filled circles, solid line agree with the fit of the original data l r Ä10 length units, dashed line. Journal of Biomechanical Engineering JUNE 2003, Vol. 125 Õ 417

4 Fig. 3 Simulated initially preloaded tendon stress-stretch data for a reference length of l r Ä10.1 representing an initially preloaded specimen open circles. Adjusted stress-stretch data and corresponding model fit filled circles, solid line agree well with the fit of the adjusted original data set l r Ä10 length units, dashed line. Note that since some information in the toe-in region is lost, agreement is not as good as with the initially slack specimen Fig. 2. very close to l 0. Thus, no correction of stretch-ratio to l 0 for these data is necessary. The data is next modified to simulate two experimental conditions, first a test of the specimen from an initially slack configuration, and second a test of the specimen from an initially significantly preloaded configuration. To simulate a specimen that is initially slack and bears no load in the reference configuration, the original data are recomputed based on a reference length of l r 9.9 length units. This is accomplished by adding a zero-load data point at l9.9 to the original load-length data, and results in a shift to the right and slight decrease in the slope of the stressstretch curve open circles, Fig. 2. Furthermore, to simulate an experiment in which a significant amount of preload is applied to the specimen, the first load-length datum point is omitted. This results in a reference length of l r length units and a shift to the left and slight increase in slope of the stress-stretch curve open circles, Fig. 3. Note that by testing from this level of preload, some of the toe-in region of the stress-stretch curve is lost. Finally, to illustrate the effect of l r on tangent modulus, the modulus is computed from the last four data points of the example data for different values of reference length ranging from l r 9.9 to l r These moduli are then recomputed based upon example data adjusted to l 0. Determining the Toe Region to Linear Region Transition Point. Once the nonlinear load-deformation or stress-stretch curve is fit with the above model, the three Weibull parameters are obtained. The point of transition from the toe region to the linear region is determined by the analytical method described below. The cumulative distribution function CDF, F(), for the Weibull distribution can be obtained by integrating the Weibull PDF, F t tps d s t The resulting CDF is s 1 exp s d s. (4) F t 1exp t (5) where F is the percentile (0F1) of area under the PDF corresponding to the magnitude of fibers in tension and carrying load. Manipulating the equation algebraically leads to the inverse CDF, t ln1f 1/. (6) Equation 6 defines the stretch ratio at which any fraction of the fibers F have been recruited. Hence, by setting F to a particular value, say 0.75 at which 75% of fibers have been recruited, one can objectively define the stretch ratio and hence strain at which a particular percentage of collagen fibers are recruited, and at which most of the fibers are recruited and the tissue exits the nonlinear strain-stiffening toe-region and enters a more linear portion of the curve. After the stretch ratio for a specific fraction of loaded fibers are determined Eq. 6, the corresponding stress may be obtained Eq. 1. Probability density functions by definition have an area under their curves equal to unity. The PDF curves in the graphical representations presented herein are scaled to the maximum attained stress in for purposes of data visualization only. No parameters are distorted during scaling, i.e., scaling does not adversely effect the Weibull parameters. The above model was applied to rat medial collateral ligament MCL stress-strain or stretch ratio data obtained from a separate 418 Õ Vol. 125, JUNE 2003 Transactions of the ASME

5 Fig. 4 Tangent modulus computed from stress-stretch data based on different choices of reference length l r white bars, and tangent modulus computed from the corresponding adjusted data gray bars. The unadjusted modulus changes linearly with l r, the adjusted modulus remains relatively constant. study, 22. These stress-stretch data from ligament are used as a further example of the application of the model to fibrous connective tissue. The stress-stretch curves used were obtained from subfailure damaged as well as contralateral control ligaments, 21. Results Tissue Reference Length. In the case of the simulated slack specimen with l r 9.9 length units, applying the model results in t The data adjusted to l 0 closely match the original data filled circles, Fig. 2. Application of the model to adjusted data results in very close agreement with the fit to the original l r 10.0 data solid versus dashed lines, Fig. 2. In the case of the preloaded specimen, applying the model results in t with a stress offset of psi. The data adjusted to l 0 also closely match the original data filled circles, Fig. 3. Again, the model applied to the adjusted data closely matches the fit to the original l r 10.0 data solid versus dashed lines, Fig. 3. Agreement is not as good as with the previous example because increasing preload results in a loss of information from the toe-in region. When further preloading eliminates most of the toe-in region from the data set, the least-squares minimization converges to nonunique solutions for the Weibull scale and shape parameters, and a consistent adjustment of the data to l 0 is not possible data not shown. Thus, too much preload results in a loss of information from the specimen such that l 0 cannot be recovered. The data show that considerable experimental bias in tangent modulus can be avoided by determining t0 and adjusting for choice of reference length Fig. 4. While the unadjusted modulus varies linearly with l r, as would be expected, the adjusted modulus remains relatively constant as reference length is increased Fig. 4. An adjusted modulus is more consistent even at relatively large preloads such as at l r i.e., up to 12% elongation relative to l 0 ) where much of the data from the toe-in region have been lost. The Toe Region to Linear Region Transition. The model fit the MCL data examined in this study extremely well (R in all cases. The stress and stretch-ratio values at the transition from the toe to linear portions of the stress-stretch curve in control and subfailure stretched MCLs were computed for a range F values Table 1. Within the assumptions of the model, F represents the ratio of collagen fibers recruited compared to total number of fibers. The larger F is, the more fibers are recruited. The Weibull parameters for the Control ligament are: 0.956, 0.019, 0.997, and for the ligament damaged by a subfailure stretch, the parameters are: 1.245, 0.021, Inspection of the data suggests that fiber recruitment over the 85th percentile provides a good indication of the transition Fig. 5. Values of F below 0.85 appear to still be well into the strain-stiffening region and therefore underestimate the transition-point from toe to linear regions. Values above an F value of 0.85 appear to describe Table 1 Tissue stress ratio t in mmõmm and stress t in MPa at the toe-region to linear region transition in control and subfailure damaged MCLs for varying values of F from 0.75 to Within the assumptions of the model, the parameter F represents a measure of the amount of collagen fiber recruitment. A larger ratio indicates more fibers have been recruited. For the connective tissue data fit in this study, the model shows that subfailure damage increases the stretch ratio and decreases the stress at which the transition occurred F t t t t t t t t t t Control Stretched Journal of Biomechanical Engineering JUNE 2003, Vol. 125 Õ 419

6 Fig. 5 Model fits for control and subfailure stretched rat MCL data from 22. The structural model proposed by Hurschler et al. 11 fit each curve with R 2Ì0.99. Note, the Weibull PDF has been scaled to the corresponding stress-stretch curve, see Methods. The Control and Damaged markers below the Stretch Ratio axis correspond to the stretch ratio calculated for a specific value of F values appear in Table 1. The tick marks represent each of the five values of F examined, starting with 0.75 and moving to the right by increments of 0.05 until the value 0.95 is reached. the transition more accurately. Of course, one can always apply a very high fiber recruitment measure i.e., 95 99% to measure the point of entire fiber recruitment, but beyond a particular threshold, say 0.85, the additional recruitment may provide only a small contribution to the strain-stiffening effect. The model reveals that subfailure damaged tissue displays an increase in the stretch-ratio or strain and a decrease in stress required for the transition when compared to the contralateral control tissue. Discussion The goal of this study was to illustrate methods in which a probabilistic microstructural model can aid in quantifying low load behaviors. Reference length of initially compliant tissues, such as tendons or ligaments, is often based on an arbitrarily assigned load threshold. These thresholds are selected more upon experimental convenience rather than physiological considerations i.e., differences between in situ and ex vivo reference length are not known due to complex geometry and loading patterns. The choice of this load threshold can bias biomechanical measures that depend on length. An objective technique for determining reference length, one that is independent of load thresholds, was therefore developed and illustrated. The technique relies on a mathematical model that assumes that fibers are recruited and bear load according to a Weibull PDF for fiber straightening as the tissue elongates, 11. Thus, it is implicitly assumed that enough low load data are present so that an accurate representation of the toe-in region is possible via the three parameters of the Weibull PDF. When insufficient toe-in data are available, it is not possible to uniquely determine the Weibull parameters, and specifically the location parameter t0, and adjustment is not possible. The technique presented herein can be applied retroactively to normalize and compare existing data. Optimally, it is applied prospectively to data that capture the toe-in region in its entirety. It eliminates entirely the need to use a load threshold i.e., 0.1 N, 1 N, or 5N to establish a reference length: the entire low-load behavior of the specimen can be captured because the specimen can be tested from an initially slack configuration. The applied microstructural model and accompanying analytical method proposed herein fit the experimental data well, and provide a parameter that can be used to consistently select a transition-point between the toe-region and the linear region in the stress-stretch curve. The parameter F defining the transition, as is the entire model, is based on the phenomenon of collagen fiber recruitment in the microstructural model. Hence, this model provides a useful tool for evaluation of experimental data, with parameters deriving from physical characteristics of the tissue. Evaluating parameters from the toe-region, as well as tangent modulus and failure parameters, allows for a more complete description of the tissue than is possible by limiting the analysis to the linear and failure regions alone. Quantifying this transitionpoint may for instance provide useful insight into the effect of experimental therapies such as mobilization and exercise, and tissue engineering methods on the recovery of normal low load strain-stiffening behavior in injured connective tissue. Furthermore, low-load behavior of connective tissues is important in daily activity and understanding and quantifying the low-load region of the stress-strain curve in connective tissue may provide insight into pathologic tissue laxity. Laxity in ligament, for example, may contribute to pathologic joint laxity, and pathologic joint laxity can lead to joint deterioration and arthritis. Quantifying the toe region to linear region transition allows for better understanding of normal tissue behavior and length and provides a baseline from which to quantify changes. The microstructure of fibrous connective tissues has a direct impact on the mechanical load-deformation and stress-stretch behaviors of the tissues. In ligament and tendon, for instance, collagen crimp drives the nonlinear strain-stiffening behavior in the low-load region when the tissue is loaded in the longitudinal direction. The stiffness of the tissue increases only as the fibers straighten and are they able to bear load. The microstructural model applied to data in this study assumes that this strainstiffening behavior is the result of collagen fiber recruitment during tissue stretch. To further examine this assumption the model was fit to the data of two existing studies, 15,23, that examine changes in collagen crimp as a function of tissue stretch Figs. 420 Õ Vol. 125, JUNE 2003 Transactions of the ASME

7 Fig. 6 Model fits to data from a Viidik 15 in which changes in collagen fiber crimp were examined with polarized light during tissue strain measured grip to grip and b Hanson et al. 23 in which changes in collagen fiber crimp were examined with optical coherence tomography during tissue strain measured grip to grip. In both cases the original units of the studies were maintained with the exception of strain being converted to stretch ratio. In the case of the Viidik data the model agrees very well, in the case of the Hanson et al. data the model slightly underpredicts the stretch at which complete fiber straightening occurs. 6a and 6b. Data were obtained from these studies, 15,23, by scanning the original figures, digitizing, and replotting the data. The model fits both data sets well (R ), and the model predicts fiber recruitment with good agreement to the experimental measures of collagen fiber straightening. In the second case Fig. 6b the measured strain at which crimp was observed to be extinguished somewhat exceeded the model prediction. It is possible that although crimp is was no longer observable using the technique in that study, that the fibers were nonetheless still not in a fully elongated state. In addition, neither study measured strain on the ligament locally, but rather grip to grip. This has been shown to increase the measured strain parameter and may therefore explain the somewhat larger toe-region strain for fiber straightening in these studies. Lastly, nonlinearities exceeding solely fiber straightening i.e., nonlinearity in the fiber themselves may be present in the tissues resulting in some small error between theory and experiment. However, the model assumes linear fiber stress-stretch which is supported by experiments performed on very small subunits of rat tail tendon, 24, and by X-ray diffractometry of bovine Achilles tendon fibril deformation, 25,26. Further study into the structure-function relationship is required. In this manuscript the proposed model was applied to tendon and ligament, although the technique could be analogously applied to other strain-stiffening fibrous connective tissue. In addition, this methodology is not restricted to the Weibull distribution, but may be implemented into other probabilistic microstructural models that utilize other PDFs. Both Gaussian and Gamma distri- Journal of Biomechanical Engineering JUNE 2003, Vol. 125 Õ 421

8 butions for fiber straightening may be capable of describing the behavior of various connective tissues with adequate fidelity, although continuous PDF s e.g., Gaussian do not yield a l 0. Once an appropriate distribution that describes tissue microstructure is selected to fit a particular data set and the data are fit, a CDF can be applied to determine the magnitude of fiber recruitment. For the data fit in this study, the 85th percentile appeared the most reasonable choice for the lower limit of transition linear region of the stress-strain curve. Values of F below 0.85 appear to be displaying substantial strain-stiffening behavior and therefore underestimate the transition-point while values above an F value of 0.85 appear to describe the transition more accurately. Above 0.85, additional fiber recruitment results in very little strainstiffening behavior, yet, one can always apply a very high fiber recruitment measure i.e., 95 99% to measure the point of entire fiber recruitment. However, the percentile used is not critical as long the value of F is fixed and reported. Once a value for F is chosen, it can be objectively applied to various groups and treatments for experimental comparison. In conclusion, the methods presented herein provide new tools with which to address some of the major difficulties associated with quantifying connective tissue low-load behavior. These tools, based on a probabilistic microstructural model for fiber straightening, now allow us objectively describe the events that govern low-load behavior, that is the initiation of load bearing and the transition from the toe to the linear region. They allow the capture of the entire low-load region of tissue behavior since the specimen can be tested from a slack configuration without the application of an arbitrary assigned preload. Acknowledgment The authors thank Dr. Dennis Heisey and Dr. Glen Leverson for their statistical insight, and Dr. David Corr for his helpful suggestions and critique. Funding for this work was provided by NASA grant # NAG and by a grant from the University of Wisconsin Surgical Associates. References 1 Lam, T. C., Shrive, N. G., and Frank, C. B., 1995, Variations in Rupture Site and Surface Strains at Failure in the Maturing Rabbit Medial Collateral Ligament, ASME J. Biomech. Eng., 1174, pp Chimich, D., Frank, C., Shrive, N., Dougall, H., and Bray, R., 1991, The Effects of Initial End Contact on Medial Collateral Ligament Healing: A Morphological and Biomechanical Study in a Rabbit Model, J. Orthop. Res., 91, pp Przybylski, G. J., Carlin, G. J., Patel, P. R., and Woo, S. L., 1996, Human Anterior and Posterior Cervical Longitudinal Ligaments Possess Similar Tensile Properties, J. Orthop. Res., 146, pp Sabiston, P., Frank, C., Lam, T., and Shrive, N., 1990, Transplantation of the Rabbit Medial Collateral Ligament. I. Biomechanical Evaluation of Fresh Autografts, J. Orthop. Res., 81, pp Woo, S. L., Gomez, M. A., Inoue, M., and Akeson, W. H., 1987, New Experimental Procedures to Evaluate the Biomechanical Properties of Healing Canine Medial Collateral Ligaments, J. Orthop. Res., 53, pp Hull, M. L., Berns, G. S., Varma, H., and Patterson, H. A., 1996, Strain in the Medial Collateral Ligament of the Human Knee Under Single and Combined Loads, erratum appears in J. Biomech, 298, pp. 1115; J. Biomech., 292, pp Fleming, B. C., Beynnon, B. D., Tohyama, H., Johnson, R. J., Nichols, C. E., Renstrom, P., and Pope, M. H., 1994, Determination of a Zero Strain Reference for the Anteromedial Band of the Anterior Cruciate Ligament, J. Orthop. Res., 126, pp Belkoff, S. M., and Haut, R. C., 1991, A Structural Model Used to Evaluate the Changing Microstructure of Maturing Rat Skin, J. Biomech., 248, pp Belkoff, S. M., and Haut, R. C., 1992, Microstructurally Based Model Analysis of Gamma-Irradiated Tendon Allografts, J. Orthop. Res., 103, pp Kastelic, J., Palley, I., and Baer, E., 1980, A Structural Mechanical Model for Tendon Crimping, J. Biomech., 1310, pp Hurschler, C., Loitz-Ramage, B., and Vanderby, Jr., R., 1997, A Structurally Based Stress-Stretch Relationship for Tendon and Ligament, ASME J. Biomech. Eng., 1194, pp Lanir, Y., 1979, A Structural Theory for the Homogeneous Biaxial Stress- Strain Relationships in Flat Collagenous Tissues, J. Biomech., 126, pp Lanir, Y., 1963, Constitutive Equations for Fibrous Connective Tissues, J. Biomech., 161, pp Kwan, M. K., and Woo, S. L., 1989, A Structural Model to Describe the Nonlinear Stress-Strain Behavior for Parallel-Fibered Collagenous Tissues, ASME J. Biomech. Eng., 1114, pp Viidik, A., 1972, Simultaneous Mechanical and Light Microscopic Studies of Collagen Fibers, Z. Anat. Entwicklungsgesch, 1362, pp Sacks, M. S., 2001, A Structural Constitutive Model for Planar Collagenous Tissues That Integrates Sals-Derived Fiber Orientation Data, Advances in Bioengineering, 51, ASME, New York. 17 Hurschler, C., Provenzano, P. P., Vanderby, Jr., R., 1998, Scanning Electron Microscopic Investigation of Healing and Normal Rat Medial Collateral Ligaments Fixed Under Slack and Loaded Conditions, Trans. Orthop. Res. Soc., 23, pp Panjabi, M. M., Yoldas, E., Oxland, T. R., and Crisco, 3rd, J. J., 1996, Subfailure Injury of the Rabbit Anterior Cruciate Ligament, J. Orthop. Res., 142, pp Weibull, W., 1951, A Statistical Distribution Function of Wide Applicability, ASME J. Appl. Mech., 183, pp Hines, W. W., and Montgomery, D. C., 1980, Probability and Statistics in Engineering and Management Science, John Wiley and Sons, New York. 21 Abrahams, M., 1967, Mechanical Behavior of Tendon in Vitro: A Preliminary Report, Med. Biol. Eng., 5, pp Provenzano, P. P., Heisey, D., Haysashi, K., Lakes, R. S., and Vanderby, Jr., R., 2002, Sub-Failure Damage in Ligament: A Structural and Cellular Evaluation, J. Appl. Physiol., 1, pp Hansen, K. A., Weiss, J. A., and Barton, J. K., 2002, Recruitment of Tendon Crimp With Applied Tensile Strain, ASME J. Biomech. Eng., 1241, pp Kato, Y. P., Christiansen, D. L., Hahn, R. A., Shieh, S.-J., Goldstein, J. D., and Silver, F. H., 1989, Mechanical Properties of Collagen Fibers: A Comparison of Reconstituted and Rat Tail Tendon Fibers, Biomaterials, 10, pp Sasaki, N., and Odajima, S., 1996, Elongation Mechanism of Collagen Fibrils and Force-Strain Relations of Tendon at Each Level of Structural Hierarchy, J. Biomech., 299, pp Sasaki, N., and Odajima, S., 1996, Stress-Strain Curve and Young s Modulus of a Collagen Molecule as Determined by The X-Ray Diffraction Technique, J. Biomech., 295, pp Õ Vol. 125, JUNE 2003 Transactions of the ASME

Nonlinear Ligament Viscoelasticity

Nonlinear Ligament Viscoelasticity Annals of Biomedical Engineering, Vol. 29, pp. 908 914, 2001 Printed in the USA. All rights reserved. 0090-6964/2001/29 10 /908/7/$15.00 Copyright 2001 Biomedical Engineering Society Nonlinear Ligament

More information

Required test duration for group comparisons in ligament viscoelasticity: A statistical approach

Required test duration for group comparisons in ligament viscoelasticity: A statistical approach Biorheology 40 (2003) 441 450 441 IOS Press Required test duration for group comparisons in ligament viscoelasticity: A statistical approach Eugene Manley, Jr. a,b, Paolo P. Provenzano a,b, Dennis Heisey

More information

Simple Shear Testing of Parallel-Fibered Planar Soft Tissues

Simple Shear Testing of Parallel-Fibered Planar Soft Tissues John C. Gardiner Jeffrey A. Weiss e-mail: jeff.weiss@utah.edu Department of Bioengineering, The University of Utah, 50 South Central Campus Drive #2480, Salt Lake City, UT 84112 Simple Shear Testing of

More information

Mathematical Modelling of Biological Soft Tissues

Mathematical Modelling of Biological Soft Tissues Mathematical Modelling of Biological Soft Tissues 1., William J. Parnell 1., Barbara Lynch 2., Hazel R.C. Screen 3. and I. David Abrahams 4. 1. University of Manchester 2. Ecole Polytechnique 3. Queen

More information

A new strain energy function for the hyperelastic modelling of ligaments and tendons

A new strain energy function for the hyperelastic modelling of ligaments and tendons A new strain energy function for the hyperelastic modelling of ligaments and tendons University of Manchester BMC-BAMC 2015 Anterior cruciate ligament reconstruction surgery Ligament and tendon hierarchical

More information

Damage Mechanics of Porcine Flexor Tendon: Mechanical Evaluation and Modeling

Damage Mechanics of Porcine Flexor Tendon: Mechanical Evaluation and Modeling Annals of Biomedical Engineering, Vol. 40, No. 8, August 2012 (Ó 2012) pp. 1692 1707 DOI: 10.1007/s10439-012-0538-z Damage Mechanics of Porcine Flexor Tendon: Mechanical Evaluation and Modeling SARAH DUENWALD-KUEHL,

More information

TINIUS OLSEN Testing Machine Co., Inc.

TINIUS OLSEN Testing Machine Co., Inc. Interpretation of Stress-Strain Curves and Mechanical Properties of Materials Tinius Olsen has prepared this general introduction to the interpretation of stress-strain curves for the benefit of those

More information

ME 2570 MECHANICS OF MATERIALS

ME 2570 MECHANICS OF MATERIALS ME 2570 MECHANICS OF MATERIALS Chapter III. Mechanical Properties of Materials 1 Tension and Compression Test The strength of a material depends on its ability to sustain a load without undue deformation

More information

Stress relaxation and recovery in tendon and ligament: Experiment and modeling

Stress relaxation and recovery in tendon and ligament: Experiment and modeling Biorheology 47 (2010) 1 14 1 DOI 10.3233/BIR-2010-0559 IOS Press Stress relaxation and recovery in tendon and ligament: Experiment and modeling Sarah E. Duenwald a, Ray Vanderby Jr. a,b and Roderic S.

More information

Mechanical behavior of Tendon and Skin 1. The nonlinear mechanical behavior of tendon. 2. The extensibility of skin.

Mechanical behavior of Tendon and Skin 1. The nonlinear mechanical behavior of tendon. 2. The extensibility of skin. Harvard-MIT Division of Health Sciences and Technology HST.523J: Cell-Matrix Mechanics Prof. Ioannis Yannas Mechanical behavior of Tendon and Skin 1. The nonlinear mechanical behavior of tendon. 2. The

More information

Linear viscoelastic behavior

Linear viscoelastic behavior Harvard-MIT Division of Health Sciences and Technology HST.523J: Cell-Matrix Mechanics Prof. Ioannis Yannas Linear viscoelastic behavior 1. The constitutive equation depends on load history. 2. Diagnostic

More information

Stress-Strain Behavior

Stress-Strain Behavior Stress-Strain Behavior 6.3 A specimen of aluminum having a rectangular cross section 10 mm 1.7 mm (0.4 in. 0.5 in.) is pulled in tension with 35,500 N (8000 lb f ) force, producing only elastic deformation.

More information

Module 5: Failure Criteria of Rock and Rock masses. Contents Hydrostatic compression Deviatoric compression

Module 5: Failure Criteria of Rock and Rock masses. Contents Hydrostatic compression Deviatoric compression FAILURE CRITERIA OF ROCK AND ROCK MASSES Contents 5.1 Failure in rocks 5.1.1 Hydrostatic compression 5.1.2 Deviatoric compression 5.1.3 Effect of confining pressure 5.2 Failure modes in rocks 5.3 Complete

More information

NOTE To improve the TA to class ratio, two groups will perform this experiment at one time. Group times are listed on the class website.

NOTE To improve the TA to class ratio, two groups will perform this experiment at one time. Group times are listed on the class website. Laboratory 3: Viscoelastic Characterization of Tendon using Harmonic Oscillations November 8/9, 2006 BIOEN 5201 Introduction to Biomechanics Instructor: Jeff Weiss TA: Heath Henninger Lab Quiz: A 10 point

More information

Development of a reduced relaxation function and comparison of stress relaxation for anatomically paired tendons

Development of a reduced relaxation function and comparison of stress relaxation for anatomically paired tendons Journal of Mechanical Science and Technology 23 (2009) 1893~1898 Journal of Mechanical Science and Technology www.springerlink.com/content/1738-494x DOI 10.1007/s12206-009-0504-3 Development of a reduced

More information

[5] Stress and Strain

[5] Stress and Strain [5] Stress and Strain Page 1 of 34 [5] Stress and Strain [5.1] Internal Stress of Solids [5.2] Design of Simple Connections (will not be covered in class) [5.3] Deformation and Strain [5.4] Hooke s Law

More information

Chapter 7. Highlights:

Chapter 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 information

2.1 Strain energy functions for incompressible materials

2.1 Strain energy functions for incompressible materials Chapter 2 Strain energy functions The aims of constitutive theories are to develop mathematical models for representing the real behavior of matter, to determine the material response and in general, to

More information

STRENGTH AND STIFFNESS REDUCTION OF LARGE NOTCHED BEAMS

STRENGTH AND STIFFNESS REDUCTION OF LARGE NOTCHED BEAMS STRENGTH AND STIFFNESS REDUCTION OF LARGE NOTCHED BEAMS By Joseph F. Murphy 1 ABSTRACT: Four large glulam beams with notches on the tension side were tested for strength and stiffness. Using either bending

More information

Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2

Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2 Samantha Ramirez, MSE Stress The intensity of the internal force acting on a specific plane (area) passing through a point. Δ ΔA Δ z Δ 1 2 ΔA Δ x Δ y ΔA is an infinitesimal size area with a uniform force

More information

Module-4. Mechanical Properties of Metals

Module-4. Mechanical Properties of Metals Module-4 Mechanical Properties of Metals Contents ) Elastic deformation and Plastic deformation ) Interpretation of tensile stress-strain curves 3) Yielding under multi-axial stress, Yield criteria, Macroscopic

More information

Lectures on. Constitutive Modelling of Arteries. Ray Ogden

Lectures on. Constitutive Modelling of Arteries. Ray Ogden Lectures on Constitutive Modelling of Arteries Ray Ogden University of Aberdeen Xi an Jiaotong University April 2011 Overview of the Ingredients of Continuum Mechanics needed in Soft Tissue Biomechanics

More information

MECE 3321 MECHANICS OF SOLIDS CHAPTER 3

MECE 3321 MECHANICS OF SOLIDS CHAPTER 3 MECE 3321 MECHANICS OF SOLIDS CHAPTER 3 Samantha Ramirez TENSION AND COMPRESSION TESTS Tension and compression tests are used primarily to determine the relationship between σ avg and ε avg in any material.

More information

Multiscale modeling of failure in ABS materials

Multiscale modeling of failure in ABS materials Institute of Mechanics Multiscale modeling of failure in ABS materials Martin Helbig, Thomas Seelig 15. International Conference on Deformation, Yield and Fracture of Polymers Kerkrade, April 2012 Institute

More information

Analysis of high loss viscoelastic composites

Analysis of high loss viscoelastic composites Analysis of high loss viscoelastic composites by C. P. Chen, Ph.D. and R. S. Lakes, Ph.D. Department of Engineering Physics Engineering Mechanics Program; Biomedical Engineering Department Materials Science

More information

BioMechanics and BioMaterials Lab (BME 541) Experiment #5 Mechanical Prosperities of Biomaterials Tensile Test

BioMechanics and BioMaterials Lab (BME 541) Experiment #5 Mechanical Prosperities of Biomaterials Tensile Test BioMechanics and BioMaterials Lab (BME 541) Experiment #5 Mechanical Prosperities of Biomaterials Tensile Test Objectives 1. To be familiar with the material testing machine(810le4) and provide a practical

More information

Load-Strength Interference

Load-Strength Interference Load-Strength Interference Loads vary, strengths vary, and reliability usually declines for mechanical systems, electronic systems, and electrical systems. The cause of failures is a load-strength interference

More information

WORKBOOK MECHANICS OF MATERIALS AND ELEMENTS OF ENGINEERING STRUCTURES

WORKBOOK MECHANICS OF MATERIALS AND ELEMENTS OF ENGINEERING STRUCTURES WORKBOOK MECHANICS OF MATERIALS AND ELEMENTS OF ENGINEERING STRUCTURES LUBLIN 014 Authors: Sylwester Samborski, Andrzej Teter and Marcin Bocheński Desktop publishing: Sylwester Samborski, Andrzej Teter

More information

ME 176 Final Exam, Fall 1997

ME 176 Final Exam, Fall 1997 Tuesday, December 16, 5:00 8:00 PM, 1997. Answer all questions for a maximum of 100 points. Please write all answers in the space provided. If you need additional space, write on the back sides. Indicate

More information

3-dimensional joint torque calculation of compression sportswear using 3D-CG human model

3-dimensional joint torque calculation of compression sportswear using 3D-CG human model 3-dimensional joint torque calculation of compression sportswear using 3D-CG human model Akihiro Matsuda, University of Tsukuba Hirokazu Tanaka, University of Tsukuba Hitoshi Aoki, University of Tsukuba

More information

Mechanical Properties of Thoracic and. Abdominal Arteries of Sheep

Mechanical Properties of Thoracic and. Abdominal Arteries of Sheep Adv. Theor. Appl. Mech., Vol. 5, 2012, no. 4, 173-178 Mechanical Properties of Thoracic and Abdominal Arteries of Sheep Kadri Salim Laboratory of Industrial Mechanic, (LMI) Department of Mechanical Engineering

More information

Cellular solid structures with unbounded thermal expansion. Roderic Lakes. Journal of Materials Science Letters, 15, (1996).

Cellular solid structures with unbounded thermal expansion. Roderic Lakes. Journal of Materials Science Letters, 15, (1996). 1 Cellular solid structures with unbounded thermal expansion Roderic Lakes Journal of Materials Science Letters, 15, 475-477 (1996). Abstract Material microstructures are presented which can exhibit coefficients

More information

Testing and Analysis

Testing and Analysis Testing and Analysis Testing Elastomers for Hyperelastic Material Models in Finite Element Analysis 2.6 2.4 2.2 2.0 1.8 1.6 1.4 Biaxial Extension Simple Tension Figure 1, A Typical Final Data Set for Input

More information

AN ANISOTROPIC PSEUDO-ELASTIC MODEL FOR THE MULLINS EFFECT IN ARTERIAL TISSUE

AN ANISOTROPIC PSEUDO-ELASTIC MODEL FOR THE MULLINS EFFECT IN ARTERIAL TISSUE XI International Conference on Computational Plasticity. Fundamentals and Applications COMPLAS XI E. Oñate, D.R.J. Owen, D. Peric and B. Suárez (Eds) AN ANISOTROPIC PSEUDO-ELASTIC MODEL FOR THE MULLINS

More information

Lab Exercise #5: Tension and Bending with Strain Gages

Lab Exercise #5: Tension and Bending with Strain Gages Lab Exercise #5: Tension and Bending with Strain Gages Pre-lab assignment: Yes No Goals: 1. To evaluate tension and bending stress models and Hooke s Law. a. σ = Mc/I and σ = P/A 2. To determine material

More information

ANSYS Mechanical Basic Structural Nonlinearities

ANSYS Mechanical Basic Structural Nonlinearities Lecture 4 Rate Independent Plasticity ANSYS Mechanical Basic Structural Nonlinearities 1 Chapter Overview The following will be covered in this Chapter: A. Background Elasticity/Plasticity B. Yield Criteria

More information

Generalized solution for predicting relaxation from creep in soft tissue: Application to ligament

Generalized solution for predicting relaxation from creep in soft tissue: Application to ligament International Journal of Mechanical Sciences 48 (26) 662 673 www.elsevier.com/locate/ijmecsci Generalized solution for predicting relaxation from creep in soft tissue: Application to ligament Ashish Oza

More information

2.1 Background of Piping Stresses

2.1 Background of Piping Stresses 2 Research Review One of the major additions to Tmin was the inclusion of analysis of a 2-Dimensional vertical piping span. The original plan from Dupont was to include several types of 2-D and 3-D vertical

More information

Tensile stress strain curves for different materials. Shows in figure below

Tensile stress strain curves for different materials. Shows in figure below Tensile stress strain curves for different materials. Shows in figure below Furthermore, the modulus of elasticity of several materials effected by increasing temperature, as is shown in Figure Asst. Lecturer

More information

CHAPTER 6 MECHANICAL PROPERTIES OF METALS PROBLEM SOLUTIONS

CHAPTER 6 MECHANICAL PROPERTIES OF METALS PROBLEM SOLUTIONS CHAPTER 6 MECHANICAL PROPERTIES OF METALS PROBLEM SOLUTIONS Concepts of Stress and Strain 6.1 Using mechanics of materials principles (i.e., equations of mechanical equilibrium applied to a free-body diagram),

More information

Exercise: concepts from chapter 8

Exercise: 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 information

Damage accumulation model for aluminium-closed cell foams subjected to fully reversed cyclic loading

Damage accumulation model for aluminium-closed cell foams subjected to fully reversed cyclic loading Fatigue & Fracture of Engineering Materials & Structures doi: 10.1111/j.1460-2695.2011.01591.x Damage accumulation model for aluminium-closed cell foams subjected to fully reversed cyclic loading H. PINTO

More information

High Tech High Top Hat Technicians. An Introduction to Solid Mechanics. Is that supposed to bend there?

High Tech High Top Hat Technicians. An Introduction to Solid Mechanics. Is that supposed to bend there? High Tech High Top Hat Technicians An Introduction to Solid Mechanics Or Is that supposed to bend there? Why don't we fall through the floor? The power of any Spring is in the same proportion with the

More information

Mechanical Properties of Materials

Mechanical Properties of Materials Mechanical Properties of Materials Strains Material Model Stresses Learning objectives Understand the qualitative and quantitative description of mechanical properties of materials. Learn the logic of

More information

The Relationship between the Applied Torque and Stresses in Post-Tension Structures

The Relationship between the Applied Torque and Stresses in Post-Tension Structures ECNDT 6 - Poster 218 The Relationship between the Applied Torque and Stresses in Post-Tension Structures Fui Kiew LIEW, Sinin HAMDAN * and Mohd. Shahril OSMAN, Faculty of Engineering, Universiti Malaysia

More information

Special edition paper

Special edition paper Development of New Aseismatic Structure Using Escalators Kazunori Sasaki* Atsushi Hayashi* Hajime Yoshida** Toru Masuda* Aseismatic reinforcement work is often carried out in parallel with improvement

More information

ME 243. Mechanics of Solids

ME 243. Mechanics of Solids ME 243 Mechanics of Solids Lecture 2: Stress and Strain Ahmad Shahedi Shakil Lecturer, Dept. of Mechanical Engg, BUET E-mail: sshakil@me.buet.ac.bd, shakil6791@gmail.com Website: teacher.buet.ac.bd/sshakil

More information

3. BEAMS: STRAIN, STRESS, DEFLECTIONS

3. BEAMS: STRAIN, STRESS, DEFLECTIONS 3. BEAMS: STRAIN, STRESS, DEFLECTIONS The beam, or flexural member, is frequently encountered in structures and machines, and its elementary stress analysis constitutes one of the more interesting facets

More information

4.MECHANICAL PROPERTIES OF MATERIALS

4.MECHANICAL PROPERTIES OF MATERIALS 4.MECHANICAL PROPERTIES OF MATERIALS The diagram representing the relation between stress and strain in a given material is an important characteristic of the material. To obtain the stress-strain diagram

More information

Full-field measurements and identification for biological soft tissues: application to arteries in vitro

Full-field measurements and identification for biological soft tissues: application to arteries in vitro Centre for Health Engineering CNRS UMR 5146 INSERM IFR 143 Prof. Stéphane Avril Full-field measurements and identification for biological soft tissues: application to arteries in vitro using single-gage

More information

Tvestigated using the quadratic form of the Tsai-Wu strength theory [I].

Tvestigated using the quadratic form of the Tsai-Wu strength theory [I]. Evaluation of Strength the TensorPolynomial Theory for Wood J. Y. L IU* Forest Products Laboratory, Forest Service U.S. Department of Agriculture, Madison, Wisconsin 53705 (Received October 10, 1983) (Revised

More information

A Constitutive Model for DYNEEMA UD composites

A Constitutive Model for DYNEEMA UD composites A Constitutive Model for DYNEEMA UD composites L Iannucci 1, D J Pope 2, M Dalzell 2 1 Imperial College, Department of Aeronautics London, SW7 2AZ l.iannucci@imperial.ac.uk 2 Dstl, Porton Down, Salisbury,

More information

CALCULATION OF A SHEET PILE WALL RELIABILITY INDEX IN ULTIMATE AND SERVICEABILITY LIMIT STATES

CALCULATION OF A SHEET PILE WALL RELIABILITY INDEX IN ULTIMATE AND SERVICEABILITY LIMIT STATES Studia Geotechnica et Mechanica, Vol. XXXII, No. 2, 2010 CALCULATION OF A SHEET PILE WALL RELIABILITY INDEX IN ULTIMATE AND SERVICEABILITY LIMIT STATES JERZY BAUER Institute of Mining, Wrocław University

More information

Statistical Comparison and Improvement of Methods for Combining Random and Harmonic Loads

Statistical Comparison and Improvement of Methods for Combining Random and Harmonic Loads 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference 19 - April 004, Palm Springs, California AIAA 004-1535 Statistical Comparison and Improvement of Methods for Combining

More information

Understanding Frequency Domain Viscoelasticity in Abaqus

Understanding Frequency Domain Viscoelasticity in Abaqus Paper # 12 Understanding Frequency Domain Viscoelasticity in Abaqus By Saurabh Bahuguna, Randy Marlow*, and Tod Dalrymple Dassault Systèmes Simulia Corp., Great Lakes Region Presented at the Fall 172 nd

More information

A concrete cylinder having a a diameter of of in. mm and elasticity. Stress and Strain: Stress and Strain: 0.

A concrete cylinder having a a diameter of of in. mm and elasticity. Stress and Strain: Stress and Strain: 0. 2011 earson Education, Inc., Upper Saddle River, NJ. ll rights reserved. This material is protected under all copyright laws as they currently 8 1. 3 1. concrete cylinder having a a diameter of of 6.00

More information

Evaluation of in-plane orthotropic elastic constants of paper and paperboard

Evaluation of in-plane orthotropic elastic constants of paper and paperboard Evaluation of in-plane orthotropic elastic constants of paper and paperboard T. Yokoyama and K. Nakai Department of Mechanical Engineering, Okayama University of Science - Ridai-cho, Okayama 7-5, Japan

More information

MATERIALS FOR CIVIL AND CONSTRUCTION ENGINEERS

MATERIALS FOR CIVIL AND CONSTRUCTION ENGINEERS MATERIALS FOR CIVIL AND CONSTRUCTION ENGINEERS 3 rd Edition Michael S. Mamlouk Arizona State University John P. Zaniewski West Virginia University Solution Manual FOREWORD This solution manual includes

More information

Module 7: Micromechanics Lecture 34: Self Consistent, Mori -Tanaka and Halpin -Tsai Models. Introduction. The Lecture Contains. Self Consistent Method

Module 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 information

Size Effects In the Crushing of Honeycomb Structures

Size Effects In the Crushing of Honeycomb Structures 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference 19-22 April 2004, Palm Springs, California AIAA 2004-1640 Size Effects In the Crushing of Honeycomb Structures Erik C.

More information

SIMPLIFIED CONCRETE MODELING WITH *MAT_CONCRET_DAMAGE_REL3

SIMPLIFIED CONCRETE MODELING WITH *MAT_CONCRET_DAMAGE_REL3 SIMPLIFIED CONCRETE MODELING WITH *MAT_CONCRET_DAMAGE_REL3 Leonard E Schwer Schwer Engineering & Consulting Services, Windsor CA, USA and L. Javier Malvar Karagozian & Case Structural Engineers, Burbank

More information

LAMINATION THEORY FOR THE STRENGTH OF FIBER COMPOSITE MATERIALS

LAMINATION THEORY FOR THE STRENGTH OF FIBER COMPOSITE MATERIALS XXII. LAMINATION THEORY FOR THE STRENGTH OF FIBER COMPOSITE MATERIALS Introduction The lamination theory for the elastic stiffness of fiber composite materials is the backbone of the entire field, it holds

More information

Design of a fastener based on negative Poisson's ratio foam adapted from

Design of a fastener based on negative Poisson's ratio foam adapted from 1 Design of a fastener based on negative Poisson's ratio foam adapted from Choi, J. B. and Lakes, R. S., "Design of a fastener based on negative Poisson's ratio foam", Cellular Polymers, 10, 205-212 (1991).

More information

VALIDATION OF PROBABILISTIC MODELS OF THE ANTERIOR AND POSTERIOR LONGITUDINAL LIGAMENTS OF THE CERVICAL SPINE

VALIDATION OF PROBABILISTIC MODELS OF THE ANTERIOR AND POSTERIOR LONGITUDINAL LIGAMENTS OF THE CERVICAL SPINE VALIDATION OF PROBABILISTIC MODELS OF THE ANTERIOR AND POSTERIOR LONGITUDINAL LIGAMENTS OF THE CERVICAL SPINE BEN H. THACKER, TRAVIS D. ELIASON, JESSICA S. COOGAN, AND DANIEL P. NICOLELLA SOUTHWEST RESEARCH

More information

ME 207 Material Science I

ME 207 Material Science I ME 207 Material Science I Chapter 3 Properties in Tension and Compression Dr. İbrahim H. Yılmaz http://web.adanabtu.edu.tr/iyilmaz Automotive Engineering Adana Science and Technology University Introduction

More information

Errors Due to Transverse Sensitivity in Strain Gages

Errors Due to Transverse Sensitivity in Strain Gages Index: Transverse Sensitivity Errors Due to Transverse Sensitivity in Strain Gages Introduction Transverse Sensitivity Table of Contents Transverse Sensitivity Errors & Their Corrections Errors Corrections

More information

Downloaded from ascelibrary.org by Colorado University at Boulder on 06/14/18. Copyright ASCE. For personal use only; all rights reserved.

Downloaded from ascelibrary.org by Colorado University at Boulder on 06/14/18. Copyright ASCE. For personal use only; all rights reserved. onlinear, Large Deformation Finite-Element Beam/Column Formulation for the Study of the Human Spine: Investigation of the Role of Muscle on Spine Stability Franck J. Vernerey 1 and Brian Moran 2 Downloaded

More information

INTRODUCTION (Cont..)

INTRODUCTION (Cont..) INTRODUCTION Name : Mohamad Redhwan Abd Aziz Post : Lecturer @ DEAN CENTER OF HND STUDIES Subject : Solid Mechanics Code : BME 2033 Room : CENTER OF HND STUDIES OFFICE H/P No. : 019-2579663 W/SITE : Http://tatiuc.edu.my/redhwan

More information

BIAXIAL STRENGTH INVESTIGATION OF CFRP COMPOSITE LAMINATES BY USING CRUCIFORM SPECIMENS

BIAXIAL STRENGTH INVESTIGATION OF CFRP COMPOSITE LAMINATES BY USING CRUCIFORM SPECIMENS BIAXIAL STRENGTH INVESTIGATION OF CFRP COMPOSITE LAMINATES BY USING CRUCIFORM SPECIMENS H. Kumazawa and T. Takatoya Airframes and Structures Group, Japan Aerospace Exploration Agency 6-13-1, Ohsawa, Mitaka,

More information

Structural behaviour of traditional mortise-and-tenon timber joints

Structural behaviour of traditional mortise-and-tenon timber joints Structural behaviour of traditional mortise-and-tenon timber joints Artur O. Feio 1, Paulo B. Lourenço 2 and José S. Machado 3 1 CCR Construtora S.A., Portugal University Lusíada, Portugal 2 University

More information

FRACTURE IN PBX 9501 AT LOW RATES

FRACTURE IN PBX 9501 AT LOW RATES FRACTURE IN PBX 9501 AT LOW RATES Cheng Liu & Richard Browning Los Alamos National Laboratory Los Alamos, NM 87545 Tensile, or mode I, fractures in PBX 9501 have a very large process zone that runs well

More information

DEVELOPMENT OF MEASURING SYSTEM FOR STRESS BY MEANS OF IMAGE PLATE FOR LABORATORY X-RAY EXPERIMENT

DEVELOPMENT OF MEASURING SYSTEM FOR STRESS BY MEANS OF IMAGE PLATE FOR LABORATORY X-RAY EXPERIMENT Copyright JCPDS - International Centre for Diffraction Data 003, Advances in X-ray Analysis, Volume 46. 6 DEVELOPMENT OF MEASURING SYSTEM FOR STRESS BY MEANS OF IMAGE PLATE FOR LABORATORY X-RAY EXPERIMENT

More information

STANDARD SAMPLE. Reduced section " Diameter. Diameter. 2" Gauge length. Radius

STANDARD SAMPLE. Reduced section  Diameter. Diameter. 2 Gauge length. Radius MATERIAL PROPERTIES TENSILE MEASUREMENT F l l 0 A 0 F STANDARD SAMPLE Reduced section 2 " 1 4 0.505" Diameter 3 4 " Diameter 2" Gauge length 3 8 " Radius TYPICAL APPARATUS Load cell Extensometer Specimen

More information

arxiv:cond-mat/ v1 25 Feb 1994

arxiv:cond-mat/ v1 25 Feb 1994 A Model for Fracture in Fibrous Materials A. T. Bernardes Departamento de Física - ICEB arxiv:cond-mat/9402110v1 25 Feb 1994 Universidade Federal de Ouro Preto Campus do Morro do Cruzeiro 35410-000 Ouro

More information

Unconfined Compression of Articular Cartilage: Nonlinear Behavior and Comparison With a Fibril-Reinforced Biphasic Model

Unconfined Compression of Articular Cartilage: Nonlinear Behavior and Comparison With a Fibril-Reinforced Biphasic Model M. Fortin Institute of Biomedical Engineering, Ecole Polytechnique, Montreal, Quebec, Canada J. Soulhat A. Shirazi-Adl Department of Mechanical Engineering, Ecole Polytechnique, Montreal, Quebec, Canada

More information

Experiment Two (2) Torsional testing of Circular Shafts

Experiment Two (2) Torsional testing of Circular Shafts Experiment Two (2) Torsional testing of Circular Shafts Introduction: Torsion occurs when any shaft is subjected to a torque. This is true whether the shaft is rotating (such as drive shafts on engines,

More information

Comparison between a Cohesive Zone Model and a Continuum Damage Model in Predicting Mode-I Fracture Behavior of Adhesively Bonded Joints

Comparison between a Cohesive Zone Model and a Continuum Damage Model in Predicting Mode-I Fracture Behavior of Adhesively Bonded Joints Copyright 2012 Tech Science Press CMES, vol.83, no.2, pp.169-181, 2012 Comparison between a Cohesive Zone Model and a Continuum Damage Model in Predicting Mode-I Fracture Behavior of Adhesively Bonded

More information

SIZE EFFECTS IN THE COMPRESSIVE CRUSHING OF HONEYCOMBS

SIZE EFFECTS IN THE COMPRESSIVE CRUSHING OF HONEYCOMBS 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Con 22-25 April 2002, Denver, Colorado SIZE EFFECTS IN THE COMPRESSIVE CRUSHING OF HONEYCOMBS Erik C. Mellquistand Anthony M.

More information

The science of elasticity

The science of elasticity The science of elasticity In 1676 Hooke realized that 1.Every kind of solid changes shape when a mechanical force acts on it. 2.It is this change of shape which enables the solid to supply the reaction

More information

Materials and Structures. Indian Institute of Technology Kanpur

Materials and Structures. Indian Institute of Technology Kanpur Introduction to Composite Materials and Structures Nachiketa Tiwari Indian Institute of Technology Kanpur Lecture 16 Behavior of Unidirectional Composites Lecture Overview Mt Material ilaxes in unidirectional

More information

EFFECT OF ALTERNATE CHANGE IN STRESS RATIO ON FATIGUE STRENGTH OF WOVEN FABRIC CFRP LAMINATE AND LIFE PREDICTION USING THE ANISOMORPHIC CFL DIAGRAM

EFFECT OF ALTERNATE CHANGE IN STRESS RATIO ON FATIGUE STRENGTH OF WOVEN FABRIC CFRP LAMINATE AND LIFE PREDICTION USING THE ANISOMORPHIC CFL DIAGRAM EFFECT OF ALTERNATE CHANGE IN STRESS RATIO ON FATIGUE STRENGTH OF WOVEN FABRIC CFRP LAMINATE AND LIFE PREDICTION USING THE ANISOMORPHIC CFL DIAGRAM M. Kawai a*, K. Yang a, S. Oh a a Department of Engineering

More information

Elastic Properties of Solids (One or two weights)

Elastic Properties of Solids (One or two weights) Elastic properties of solids Page 1 of 8 Elastic Properties of Solids (One or two weights) This is a rare experiment where you will get points for breaking a sample! The recommended textbooks and other

More information

1 Slope Stability for a Cohesive and Frictional Soil

1 Slope Stability for a Cohesive and Frictional Soil Slope Stability for a Cohesive and Frictional Soil 1-1 1 Slope Stability for a Cohesive and Frictional Soil 1.1 Problem Statement A common problem encountered in engineering soil mechanics is the stability

More information

ESTIMATION OF THE SMALL-STRAIN STIFFNESS OF GRANULAR SOILS TAKING INTO ACCOUNT THE GRAIN SIZE DISTRIBUTION CURVE

ESTIMATION OF THE SMALL-STRAIN STIFFNESS OF GRANULAR SOILS TAKING INTO ACCOUNT THE GRAIN SIZE DISTRIBUTION CURVE 5th International Conference on Earthquake Geotechnical Engineering, January 211, 1-13, Santiago, Chile. ESTIMATION OF THE SMALL-STRAIN STIFFNESS OF GRANULAR SOILS TAKING INTO ACCOUNT THE GRAIN SIZE DISTRIBUTION

More information

Compact energy absorbing cellular structure

Compact energy absorbing cellular structure Structures Under Shock and Impact IX 413 Compact energy absorbing cellular structure M. Ali 1, A. Qamhiyah 2, D. Flugrad 1 & M. Shakoor 1 1 Department of Mechanical Engineering, Iowa State University,

More information

DEVELOPMENT OF AUTOMATIC CONTROL OF MULTI-STAGE TRIAXIAL TESTS AT THE UNIVERSITY OF MISKOLC

DEVELOPMENT OF AUTOMATIC CONTROL OF MULTI-STAGE TRIAXIAL TESTS AT THE UNIVERSITY OF MISKOLC Geosciences and Engineering, Vol. 2, No. 3 (2013), pp. 37 43. DEVELOPMENT OF AUTOMATIC CONTROL OF MULTI-STAGE TRIAXIAL TESTS AT THE UNIVERSITY OF MISKOLC BALÁZS CSUHANICS ÁKOS DEBRECZENI Institute of Mining

More information

Solid Mechanics Chapter 1: Tension, Compression and Shear

Solid Mechanics Chapter 1: Tension, Compression and Shear Solid Mechanics Chapter 1: Tension, Compression and Shear Dr. Imran Latif Department of Civil and Environmental Engineering College of Engineering University of Nizwa (UoN) 1 Why do we study Mechanics

More information

A novel elastometer for soft tissue

A novel elastometer for soft tissue Computational Methods and Experiments in Material Characterisation II 111 A novel elastometer for soft tissue S. M. Harrison 1, M. B. Bush 1 & P. Petros 1,2 1 University of Western Australia 2 Royal Perth

More information

Module 7: Micromechanics Lecture 29: Background of Concentric Cylinder Assemblage Model. Introduction. The Lecture Contains

Module 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 information

Chapter 2: Deflections of Structures

Chapter 2: Deflections of Structures Chapter 2: Deflections of Structures Fig. 4.1. (Fig. 2.1.) ASTU, Dept. of C Eng., Prepared by: Melkamu E. Page 1 (2.1) (4.1) (2.2) Fig.4.2 Fig.2.2 ASTU, Dept. of C Eng., Prepared by: Melkamu E. Page 2

More information

Discussion: behaviour of jacked and driven piles in sandy soil

Discussion: behaviour of jacked and driven piles in sandy soil Title Discussion: behaviour of jacked and driven piles in sandy soil Author(s) Yang, J; Tham, LG; Lee, PKK; Chan, ST; Yu, F Citation Géotechnique, 27, v. 7 n., p. 47-478 Issued Date 27 URL http://hdl.handle.net/1722/7161

More information

Experiment Five (5) Principal of Stress and Strain

Experiment Five (5) Principal of Stress and Strain Experiment Five (5) Principal of Stress and Strain Introduction Objective: To determine principal stresses and strains in a beam made of aluminum and loaded as a cantilever, and compare them with theoretical

More information

Comparison of Ogden Two-network and Ogden Three-network Model as a Replacement for Kelvin Model in the Posture Module

Comparison of Ogden Two-network and Ogden Three-network Model as a Replacement for Kelvin Model in the Posture Module The National Center for Voice and Speech Online Technical Memo No.14, Apr. 12, version 2. Comparison of Ogden Two-network and Ogden Three-network Model as a Replacement for in the Posture Module Sree Harsha

More information

Task 1 - Material Testing of Bionax Pipe and Joints

Task 1 - Material Testing of Bionax Pipe and Joints Task 1 - Material Testing of Bionax Pipe and Joints Submitted to: Jeff Phillips Western Regional Engineer IPEX Management, Inc. 20460 Duncan Way Langley, BC, Canada V3A 7A3 Ph: 604-534-8631 Fax: 604-534-7616

More information

Evaluation of Flexural Stiffness for RC Beams During Fire Events

Evaluation of Flexural Stiffness for RC Beams During Fire Events 3 rd International Structural Specialty Conference 3 ième conférence internationale spécialisée sur le génie des structures Edmonton, Alberta June 6-9, 202 / 6 au 9 juin 202 Evaluation of Flexural Stiffness

More information

ME 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 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 information

On the Constitutive Models for Heart Valve Leaflet Mechanics

On the Constitutive Models for Heart Valve Leaflet Mechanics Cardiovascular Engineering: An International Journal, Vol. 5, No. 1, March 005 ( C 005) DOI: 10.1007/s10558-005-307-x On the Constitutive Models for Heart Valve Leaflet Mechanics ELI J. WEINBERG and MOHAMMAD

More information

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains STRENGTH OF MATERIALS-I Unit-1 Simple stresses and strains 1. What is the Principle of surveying 2. Define Magnetic, True & Arbitrary Meridians. 3. Mention different types of chains 4. Differentiate between

More information

7.6 Stress in symmetrical elastic beam transmitting both shear force and bending moment

7.6 Stress in symmetrical elastic beam transmitting both shear force and bending moment 7.6 Stress in symmetrical elastic beam transmitting both shear force and bending moment à It is more difficult to obtain an exact solution to this problem since the presence of the shear force means that

More information

STRAIN GAUGES YEDITEPE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING

STRAIN GAUGES YEDITEPE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING STRAIN GAUGES YEDITEPE UNIVERSITY DEPARTMENT OF MECHANICAL ENGINEERING 1 YEDITEPE UNIVERSITY ENGINEERING FACULTY MECHANICAL ENGINEERING LABORATORY 1. Objective: Strain Gauges Know how the change in resistance

More information