332: Mechanical Behavior Of Materials - Northwestern University

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332: Mechanical Behavior of MaterialsDepartment of Materials Science and EngineeringNorthwestern UniversityJuly 21, 2022Contents1Catalog Description42Course Outcomes43Introduction64Stress and Strain4.1 Tensor Representation of Stress4.2 Tensor Transformation Law . .4.3 Principal Stresses . . . . . . . .4.4 Strain . . . . . . . . . . . . . . .4.5 Deformation Modes . . . . . . .4.6 Representative Moduli . . . . .4.7 Speed of Sound . . . . . . . . .77914232733335Matrix Representation5.1 Compliance matrix . . . . . . . . . . . . . . . . . . . . . . . . . .5.2 Stiffness Matrix . . . . . . . . . . . . . . . . . . . . . . . . . . . .5.3 Symmetry Requirements . . . . . . . . . . . . . . . . . . . . . . .353536366Other Symmetry-Related Constitutive Relationships447Contact Mechanics7.1 Sign conventions . . . . . . . . .7.2 Flat Punch Indentation . . . . . .7.3 Energy Release Rate . . . . . . .7.4 Contact of Paraboloids . . . . . .7.5 Indentation with Berkovich Trips8Fracture.464647495861641

CONTENTS8.18.28.38.48.58.68.78.89CONTENTSFracture Modes . . . . . . . . . . . . .Stress Concentrations . . . . . . . . . .Stress Intensity Factor . . . . . . . . .Fracture condition . . . . . . . . . . . .General relationship between K and GSome Specific Geometries . . . . . . .Fracture Toughness of Materials . . . .Case Studies in Fracture . . . . . . . .Weibull Analysis of Failure64656669707175778310 Toughening Mechanisms10.1 Hydraulic Fracturing (Fracking) . . . . . . . . . . . . . . . . . .868611 Yield Behavior11.1 Critical Resolved Shear Stress . . . . . . . . . . . . . . . . . . . .11.2 Yield Surfaces . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11.3 Localized Deformation . . . . . . . . . . . . . . . . . . . . . . . .8888909312 Deformation Twinning9913 Strengthening of Metals13.1 Dislocation Basics . . . . . . . .13.2 Dislocation Interactions . . . .13.3 Work Hardening . . . . . . . .13.4 Grain Boundary Strengthening13.5 Precipitation Hardening . . . .13.6 Solid Solution Strengthening .10110210210610610710714 High Temperature Creep14.1 Dislocation Glide . . . . . . . . . . . . . . . . . . . . . .14.2 Nabarro-Herring Creep: Bulk Diffusion Within a Grain14.3 Coble Creep: Grain Boundary Diffusion . . . . . . . . .14.4 Weertman model of Creep by Dislocation Climb . . . .14.5 Deformation mechanism maps . . . . . . . . . . . . . .108111112114115115.15 Deformation of Polymers11716 Linear Viscoelasticity12616.1 Time-Dependent Moduli . . . . . . . . . . . . . . . . . . . . . . . 12617 Creep Behavior17.1 Linear Creep . . . . . . . . . . . . . . .17.2 Nonlinear Creep . . . . . . . . . . . . .17.3 Use of empirical, analytic expressions17.4 Eyring Model of Steady State Creep .2.129129130131132

CONTENTSCONTENTS18 Materials Selection19 Review Questions19.1 Stress and Strain . .19.2 Linear Elasticity . .19.3 Fracture Mechanics19.4 Yield Behavior . . .19.5 Viscoelasticity . . .19.6 Creep . . . . . . . .136.14114114114114214314320 Finite Element Analysis20.1 The direct stiffness method . . .20.2 Preliminaries . . . . . . . . . . . .20.3 Example Problem . . . . . . . . .20.4 Going further with Abaqus/CAE.143144151157160.Nomenclature16321 Python Code Examples16422 332 Problems22.1 Course Organization . . . . . . . . . . . . .22.2 The Stress Tensor . . . . . . . . . . . . . . .22.3 Strains . . . . . . . . . . . . . . . . . . . . .22.4 Typical Moduli . . . . . . . . . . . . . . . .22.5 Matrix Representation of Stress and Strains22.6 Other Linear Properties . . . . . . . . . . . .22.7 Yield Criteria . . . . . . . . . . . . . . . . . .22.8 Strengthening Mechanisms . . . . . . . . .22.9 Contact Mechanics . . . . . . . . . . . . . .22.10Nanoindentation . . . . . . . . . . . . . . .22.11Fracture Mechanics . . . . . . . . . . . . . .22.12Weibull Statistics . . . . . . . . . . . . . . .22.13Viscoelasticity . . . . . . . . . . . . . . . . .22.14Nonlinear Viscoelasticity and Creep . . . .16716716716816816817017117417717817918218218623 332 Laboratories18923.1 L1-C: Cantilever Beam . . . . . . . . . . . . . . . . . . . . . . . . 18923.2 L3-C: Stress Concentrator . . . . . . . . . . . . . . . . . . . . . . 19323.3 L3-E: Mechanical Testing of Materials - Lab and Final Project . . 202Nomenclature2083

21COURSE OUTCOMESCatalog DescriptionPlastic deformation and fracture of metals, ceramics, and polymeric materials;structure/property relations. Role of imperfections, state of stress, temperatures, strain rate. Lectures, laboratory. Prerequisites: 316 1; 316 2 (may betaken concurrently).2Course OutcomesAt the conclusion of the course students will be able to:1. Apply basic concepts of linear elasticity, including multiaxial stressstrain relationships through elastic constants for single and polycrystals.2. Quantify the different strengthening mechanisms in crystalline materials, based on interactions between dislocations and obstacles, such as:point defect (solid solution strengthening), dislocations (work hardening), grain boundaries (boundary strengthening) and particles (precipitation and dispersion strengthening).3. Apply fracture mechanics concepts to determine quantitatively when existing cracks in a material will grow.4. Describe how composite toughening mechanisms operate in ceramic matrix and polymer matrix composties.5. Derive simple relationships for the composite stiffness and strengthbased on those of the constituent phases.6. Exhibit a quantitative understanding of high temperature deformationin metals and ceramics, based on various creep mechanisms relate to diffusional and dislocation flow (Coble, Nabarro-Herring and Dislocationcreep/climb mechanisms).7. Exhibit a basic understanding of factors affecting fatigue in engineeringmaterials, as related to crack nucleation and propagation, as well as theirconnection to macroscopic fatigue phenomena.8. Describe the interplay between surface phenomena (environmental attack) and stresses leading to material embrittlement.9. Use the finite element method to calculate the stress and strain statesfor simple test cases, including a cantilever beam and a material with acirculat hole that is placed in tension.10. Use complex moduli to solve mechanics problems involving an oscillatory stress.4

2COURSE OUTCOMES11. Prepare and characterize specimens for measurement of mechanicalproperties.12. Write results from a laboratory project in the form of a journal article,and present their work orally as would be required in a technical forum.13. Select materials based on design requirements.5

33INTRODUCTIONIntroductionIn Figure 3.1, we show the materials available to mankind from the beginningof time until the current day.[1] The data are plotted as so-called ’Ashby plots’,where two material properties are chosen for the x and y axes. In Figure 3.1we use density to separate different materials along the x axis, and the fracturestrength, σ f , to separate materials on the y axis. When the story begins, allwe had to work with are the materials we could find around us or dig out ofthe ground. Over time, we Figure d out how to produce more materials forall kinds of purposes. The biggest developments come after World War II, asituation that coincides with the emergence of materials science as a discipline.We no longer rely on empiricism for materials development, but can actuallybegin to design new materials with the properties we want, or at least designmaterials that re better than anything we had before. The principles underlying the development of materials with the mechanical response forms thebasis for this course.Figure 3.1: Available materials throughout history (from ref.[1]).6

4STRESS AND STRAINyxFigure 4.1: 2-dimensional stress tensor4Stress and StrainThe mechanical properties of a material are defined in terms of the strain response of material after a certain stress is applied. In order to properly understand mechanical properties, we have to have a good understanding of stressand strain, so that’s where we begin.Some Notes on Notation: There are different ways to represent scalarquantities, vectors and matrices. Here’s how we do it in this text: Scalar quantities are straight up symbols, like P1 , σ12 , etc. Vectors are indicated with an arrow over the symbol, like P. Unit vectors are indicated with a caret above the symbol, like n̂. Matrices are enclosed in square brackets, like [σ ]4.1Tensor Representation of StressThe stress applied to an object, which we denote as σij or [σ ] is the force actingover an area of an object, divided by the area over which this force is acting.Note note that [σ ] is a matrix with individual components, σij specified by theindices i and j. These indices have the following significance: i: surface normal (i x, y, z) j: direction of force (j x, y, z)To obtain the Engineering stress, [σeng ], we use the undeformed areas of thestress-free object to obtain the stress tensor, whereas the true stress (which is7

4.1Tensor Representation of Stress4STRESS AND STRAINwhat we generally mean when we write [σ ]) we use the actual areas in theas-stressed state.The stress matrix is a tensor, which means that it obeys the coordinate transformation laws describe below. In two dimensions it has the following form: [σ] σxxσyxσxyσyy (4.1)The stress tensor must be symmetric, with σxy σyx . If this were not thecase, the torques on the volume element shown above in Figure 4.1 wouldnot balance, and the material would not be in static equilibrium. As a resultthe two dimensional stress state is specified by three components of the stresstensor: 2 normal stresses, σxx , σyy . These are referred to as ’normal’ stresses because the force acts perpendicular to the plane that it is referred to. A single shear stress, σxy .In three dimensions we add a z axis to the existing x and y axes, so the stressstate is defined by a symmetric 3x3 tensor. The full stress tensor can be used todefine the stresses acting on any given plane. To simplify the notation a bit welabel the three orthogonal directions by numbers (1, 2 and 3) instead of letters(x, y and z). The stress tensor gives the components of the force (P1 , P2 and P3 )acting on a given plane. The plane is specified by the orientation of the unitvector, n̂ that is perpendicular to the plane. This vector has components n1 , n2and n3 in the 1, 2 and 3 directions, respectively. It’s a ’unit’ vector because the 1/2length of the vector is 1, i.e. n21 n22 n23 1. The relationship between P, σ and n is as follows: P1σ11 P2 A σ12P3σ13σ12σ22σ23 σ13n1σ23 n2 σ33n3(4.2)or in more compact matrix notation: P A [σ] n̂(4.3)Here A is the total cross sectional area of the plane that we are interested in. (Ifyou need a refresher on matrix multiplication, the Wikipedia page on MatrixMultiplication (https://en.wikipedia.org/wiki/Matrix multiplication)[2] is very helpful).8

4STRESS AND STRAIN4.2Tensor Transformation Law312Figure 4.2: 3 dimensional stress tensorIn graphical form the relationship is as shown in Figure 4.2. Like the 2dimensional stress tensor mentioned above, the 3-dimensional stress tensormust also be symmetric in order for static equilibrium to be achieved. Thereare therefore 6 independent components of the three-dimensional stress tensor: 3 normal stresses, σ11 , σ22 and σ33 , describing stresses applied perpendicular to the 1, 2 and 3 faces of the cubic volume element. 3 shear stresses: σ12 , σ23 and σ13 .The three dimensional stress tensor is a 3x3 matrix with 9 elements (thoughonly 6 are independent), corresponding to the three stress components actingon each of the three orthogonal faces of cube in the Cartesian coordinate system used to define the stress components. The 1 face has n1 1, n2 0 andn3 0. By setting n (1, 0, 0) in Eq. 4.2, we get the following for the stressesacting on the 1 face of the volume element:P1 /A σ11P2 /A σ12P3 /A σ13(4.4)Equivalent expressions can be obtained for the stresses acting on the 2 and 3faces, by setting n (0, 1, 0) and n (0, 0, 1), respectively.4.2Tensor Transformation LawThe stress experienced by a material does not depend on the coordinate system used to define the stress state. The stress tensor will look very different ifwe chose a different set of coordinate axes to describe it, however, and it is important to understand how changing the coordinate system changes the stresstensor. We begin in this section by describing the procedure for obtaining the9

4.2Tensor Transformation Law422'2'2222'12'12'1212113STRESS AND STRAIN111'113' 3Figure 4.3: Rotation of coordinate system. The coordinate system is rotated byθabout the 3 axis, transforming the 1 axis to10 and the 2 axis to20 .stress tensor that emerges from a given change in the coordinate system. Wethen describe the method for obtaining a specific set of coordinate axis whichgives a diagonalized tensor where only normal stresses are present (Section4.3).4.2.1Specification of the Transformation MatrixIn general, we consider the case where our 3 axes (which we refer to simply asaxes 1, 2 and 3) are moved about the origin to define a new set of coordinateaxes that we refer to as 10 , 20 and 30 . As an example, consider the simple counterclockwise rotation around the 3 axis by an angle φ, shown schematically inFigure 4.3. In general, the relative orientation of the transformed (rotated) anduntransformed coordinate axes are given by a set of 9 angles between the 3untransformed axes and the three transformed axes. In our notation we specify these angles as θij , where i specifies the transformed axes (10 , 20 or 30 ) and jspecifies the untransformed axis (1, 2 or 3). In our simple example, the anglebetween the 1 and 10 axes is φ, so θ11 φ. The angle between the 2 and 20 axesis also φ, so θ22 φ. The 3 axis remains unchanged in our rotation example,so θ33 0. The 3/30 axis remains perpendicular to the 1,10 , 2,20 axes, so wehave θ31 θ32 θ13 θ23 90 . Finally, we see that the angle between the 10and the 2 axis is 90 φ (θ12 90 φ) and the angle between the 20 and 1 axisis 90 φ (θ21 90 φ). The full [θ ] matrix in this case is as follows: φ90 φ 90φ90 (4.5)[θ ] 90 φ90900Note that the [θ ] matrix is NOT symmetric (θij 6 θ ji ), so you always need tomake sure the first index, i, (denoting the row in the [θ ] matrix) corresponds tothe transformed axes, and the second index, j (denoting the column in the [θ ]matrix) corresponds to the original, untransformed axes.10

4STRESS AND STRAIN4.2.24.2Tensor Transformation LawExpressions for the Stress ComponentsOnce we specify all the different components of [θ ], we can use the following general expression to obtain the stresses in the new (primed) coordinatesystem as a function of the stresses in the original coordinate system:σij0 cos θ jk cos θil σkl(4.6)k,lFor each component of the stress tensor, we have to sum 9 individual terms0 is given as follows:(all combinations of k and l from 1 to 3). For example, σ120 cos θ cos θ σ cos θ cos θ σ cos θ cos θ σ σ122111 112112 122113 13cos θ22 cos θ11 σ21 cos θ22 cos θ12 σ22 cos θ22 cos θ13 σ23 cos θ23 cos θ11 σ31 cos θ23 cos θ12 σ32 cos θ23 cos θ13 σ33(4.7)The calculation is breathtakingly tedious if we do it all by hand, so it makessense to automate this and do the calculation via computer, in our case withPython. In this example we’ll start with a simple stress state corresponding touniaxial extension in the 1 direction, with the following untransformed stresstensor:5x106 [σ] 00 0 00 0 0 0(4.8)Suppose we want to obtain the stress tensor in the transformed coordinatesystem obtained from a 45 counterclockwise rotation around the z axis. Therotation matrix is given by Eq. 4.5, with φ 45 . The following Python codesolves for the full transformed tensor, with σij given by Eq. 4.8 and θij givenby Eq. 4.5 with φ 45 :12#!/ usr / bin / env python3# -* - coding : utf -8 -* -34import numpy as np567sig np . zeros ((3 , 3) ) # % create stress tensor and set to zerosig [0 , 0] 5 e6 ; # this is the only nonzero component89sigp np . zeros ((3 , 3) ) # initalize rotated streses to zero1011phi 451213theta [[ phi ,90 - phi ,90] , [90 phi , phi ,90] , [90 ,90 ,0]]11

4.2Tensor Transformation Law4STRESS AND STRAINFigure 4.4: Output generated by rotate45.py.141516171819theta np . deg2rad ( theta ) # trig functions need angles inradiansfor i in [0 , 1 , 2]:for j in [0 , 1 , 2]:for k in [0 , 1 , 2]:for l in [0 , 1 , 2]:sigp [i , j ] sigp [i , j ] np . cos ( theta [i , k ]) * np . cos (theta [j , l ]) * sig [k , l ]2021print ( sigp )# display the transformed tensor componentsWe use Python because it is free, powerful, and quite easy to learn especiallyif you have experience with a similarly-structured programming environmentlike MATLAB. Various Python code examples are included in this text, and arepresented as examples of how to do some useful things in Python.The output generated by the Python code is shown in Figure 4.4, and corresponds to the following result: 2.5x106 0 σ 2.5x1060 2.5x1062.5x1060 00 0(4.9)Note the following: The normal stresses in the 1 and 2 directions are equal to one another. The transformed shear stress in the 1-2 plane is half the original tensilestress. The sum of the normal stresses (the sum of the diagonal components ofthe stress tensor) is unchanged by the coordinate transformation4.2.3An Easier Way: Transformation by Direct Matrix MultiplicationA much easier way to do the transformation is to use a little bit of matrix math.The approach we use is described in a very nice web page put together by Bob12

4STRESS AND STRAIN4.2Tensor Transformation LawMcGinty[3]: A transformation matrix, Qij , is obtained by taking the cosinesof all of these angles describing the relationship between the transformed anduntransformed coordinate axes:[Q] cos [θ ](4.10)For the simple case of rotation about the z axis, the angles are given by Eq. 4.5,so that [Q] is given as: cos φ[Q] cos (90 φ)cos 90cos (90 φ)cos φcos 90 cos 90cos φcos 90 sin φcos 00sin φcos φ0 00 1(4.11)The transformed stress is now obtained by the following simple matrix multiplication: 0 σ [Q] [ σ ] [Q] T(4.12)where the[Q] T is the transpose of[Q]:Q T (i, j) Q( j, i )(4.13)For the rotation by φ around the z axis, [Q] T is given by the following: cos φ[Q] T sin φ0 sin φ 0cos φ 0 01(4.14)Equation 4.12 is much easier to deal with than Eq. 4.7. The Python code to takea uniaxial stress state and rotate the coordinate system by 45 about the 3 axislooks like this if we base it on Eq. 4.12:1import numpy as np234# create stress tensor with all zero elementssig np . zeros ((3 ,3) )567# set first one elment to be nonzero ( one of the normal stresses )sig [0][0] 5 e68910# set the rotation anglephi 45111213# define the rotation matrix in degreestheta np . array ([[ phi ,90 phi ,90] ,[90 - phi , phi ,90] ,[90 ,90 ,0]])13

4.3Principal Stresses4STRESS AND STRAINFigure 4.5: Principal Stresses141516# now put all the direction cosines in QQ np . cos ( np . radians ( theta ) )171819# claculate the transpose of QQT np . transpose ( Q )20212223# now multiply everything together# note that we use the @ sign to multiply matrices in pythonsigp np . round ( Q@sig@QT )242526# print the resultprint ( sigp )Running this script gives the output shown in Figure 4.4, i.e. we obtain exactlythe same result we obtained by using Eq. 4.7.4.3Principal StressesAny stress state (true stress) can be written in terms of three principal stressespppσ1 , σ2 and σ3 , applied in three perpendicular directions as illustrated in Figure 4.5. Note that we still need 6 independent parameters to specify a stressstate: the 3 principal stresses, in addition to three parameters that specify theorientation of the principal axes. The stress tensor depends on our definitionof the axes, but it is always possible to chose the axes so that all of the shearcomponents of the stress tensor vanish, so that the stress tensor looks like thefollowing: pσ1[σ] 000pσ20 00 pσ3(4.15)In order to gain some insight into the points mentioned above, it is usefulto consider a range of rotation angles, and not just a singe rotation angle of45 . One way to do this is to use the symbolic math capability of Python (or14

4STRESS AND STRAIN4.3Principal Stressesyour other favorite software) to obtain the full stress tensor as a function of therotation angle. We’ll use the principal axes to define our untransformed state,and transform to a new set of axes by rotating counterclockwise by an angle φaround the 3 axis. We want to calculate[σ0 ] from Eqs.4.11 and 4.12 as we did before, but we leave φ as an independentvariable. We use the following python script to do this:123# mohr circle . py# Mohr 's circle derivationfrom sympy import symbols , Matrix , cos , pi , simplify , preview4567# specify the principal stressesSsig1p , sig2p , sig3p symbols ([ ' sigma 1 p ' , ' sigma 2 p ' , ' sigma 3 p ' ])sig Matrix ([[ sig1p , 0 , 0] , [0 , sig2p , 0] , [0 , 0 , sig3p ]])8910# now specify the rotation anglephi symbols ( ' phi ')111213# specify the theta matrixtheta Matrix ([[ phi , pi /2 - phi , pi /2] , [ pi /2 phi , phi , pi /2] ,[ pi /2 , pi/2 ,0]])141516# take the cosine of all the elements in the matrix to get QQ theta . applyfunc ( cos )171819# get the transpose of the matrixQT Q . transpose ()202122# now do the matrix m ultipl icatio n to get the transformed matrixsigp Q * sig * QT23242526# now simplify and show the outputexp1 simplify ( sigp )preview ( exp1 , filename ' ./ figures / sy mpy m o hr e x p1 . svg ')272829# define the center ( C ) and radius ( R ) of the circleR , C symbols ([ 'R ' , 'C ' ])30313233# now we rewrite in terms of center and radius and simplify againsigp sigp . subs ([( sig1p , C R ) , ( sig2p , C - R ) ])exp2 simplify ( sigp )34353637# now save the exp1 and exp2 as image filespreview ( exp1 , viewer ' file ' , filename ' ./ figures /s ym py mo hr ex p1 . png ')preview ( exp2 , viewer ' file ' , filename ' ./ figures /s ym py mo hr ex p2 . png ')This results in the following expression for [σ0 ] (exp1, generated in line 26 ofmohr circle.py).15

4.3Principal Stresses4STRESS AND STRAINThis is not yet a very illuminating result, but it is the basis for the Mohr circleconstruction, which provides a very useful way to visualize two dimensionalstress states. This construction is described in more detail in the followingSection.4.3.1Mohr’s Circle ConstructionThe Mohr circle is a graphical construction that can be used to describe atwo dimensional stress state. A two dimensional stress state is specified bypptwo principal stresses, σ1 and σ2 , and by the orientation of the principalppaxes. The Mohr circle is drawn with a radius, R, of σ1 σ2 , centered atC ppσ1 σ2 /2 on the horizontal axis. We can use these values of R andC as the independent variables in the expression for σ0 that we obtained fromour python script. This substitution is made in lines 30-34 of mohr circle.py,and leads to the following expression for [σ0 ] (exp2 from line 34):Python has taken us almost as far as we need to go, but it doesn’t seem to besmart enough to use the following two trigonometric identities:1 2 sin2 φ cos (2φ)1 2 cos2 φ cos (2φ)(4.16)Substituting these into the expression for [σ0 ] gives our final result: C R cos (2φ) 0 σ R sin (2φ)0 R sin (2φ)0C R cos (2φ) 0 p0φ3(4.17)In the Mohr circle construction normal stresses (σN ) are plotted on the x axisand the shear component of the stress tensor (τ) is plotted on the y axis. Fora two dimensional stress state in the 1-2 plane the circle is defined by twopoints: (σ11 , σ12 ) and (σ22, σ12 ). In our current example the stress state in16

4STRESS AND STRAIN4.3Principal StressesFigure 4.6: Mohr’s circle construction.the untransformedaxesrepresentedby the open symbols in Figure 4.6, i.e. is ppby the points σ1 , 0 and σ1 , 0 . In the transformed axes the stress state isrepresented by the solid circles in Figure 4.6. From Eq. 4.17 it is evident thatthe relationship between the two different representations of the stress state isobtained by a rotation along circle by 2φ. Whether this rotation is clockwiseor counterclockwise depends on the sign convention in the definition of theshear stress. We’re not going to worry about it here, but you can refer to theMohr’s Circle Wikipedia article[4] for the details (see the Section on the signconvention).The Mohr circle construction can only be applied for a two dimensional meaning that there are no shear stresses with a component in the direction of therotation axis. There can be a normal stress in the third direction, as in our example above, because this normal stress is simply superposed on the 2d stresspppstate. In general, there are three principal stresses, σ1 , σ2 and σ3 , and we candraw the Mohr circle construction with any combination of these 3 stresses. Weend up with 3 different circles, as shown in Figure 4.7. Note that the convenpption is that σ1 is the largest principal stress and that σ3 is the smallest principalpppstress, i.e. σ1 σ2 σ3 . An important result is that the largest shear stress,τmax , is given by the difference between the largest principal stress and thesmallest one:τmax 1 ppσ1 σ32(4.18)This maximum shear stress is an important quantity, because it determineswhen a material will deform plastically (much more on this later). In order17

4.3Principal Stresses4STRESS AND STRAINFigure 4.7: Three-dimensional Mohr’s Circle.to determine this maximum shear stress, we need to first Figure out what theprincipal stresses are. In some cases this is easy. In a uniaxial tensile test, one ofthe principals stresses is the applied stress, and the other two principal stressesare equal to zero.The individual Mohr’s circles in Figure 4.7 correspond to rotations in thearound the individual principal axes. Circle C1 corresponds to rotation aroundpthe direction in which σ1 is directed, C2 corresponds to rotation around thepdirection in which σ2 is directed, and C3 corresponds to rotation around thepdirection in which σ3 is directed. A consequence of this is that is always possible to use the Mohr’s circle construction to determine the principal stresses ifthere is only one non-zero shear stress.1) Exercise:state:Determine the maximum shear stress for the following stress 3[σ] 02030 20 MPa5(4.19)2) Solution:We can handle this one without using a computer. Thereis only one non-zero shear stress (σ13 ), so we can determine the principals18

4STRESS AND STRAIN4.3Principal Stressesstresses in the following manner:1. One of the three principal stresses is the normal stress in the directionthat does not involve either of the directions in the nonzero shear stress.Since the non-zero shear stress in our example is σ13 , one of the principal stresses is σ22 3 MPa.2. Now we draw a Mohr circle construction using the two normal stressesand the non-zero shear stress, in this case σ11 , σ33 and σ13 . Mohr’s circleis centered at the the average of these two normal stresses, in our caseat C (σ11 σ33 ) /2 4 MPa.3. Determine the radius of the circle, R, is given as:R q2 (σ33 σc )2 σ13q2 2.24 MPa(5 4)2 σ134. The principal stresses are given by the intersections of the circle withthe horizontal axis:σ p C R 6.24 MPa, 1.76 MPaThe third principal stress is 3 MPa, as we already determined.5. The maximum shear stress is half the difference between the largestprincipal stress (6.64 MPa) and the smallest one (1.76), or 2.24 MPa.4.3.2Critical Resolved Shear Stress for Uniaxial TensionAs an example of the Mohr circle construction we can consider the calculation of the resolved shear stress on a sample in a state of uniaxial tension. TheMohr’s circle representation of the stress state is shown in Figure 4.8. The resolved shear stress, τrss , for sample in uniaxial tension is given by the followingexpression:19

4.3Principal Stresses4STRESS AND STRAINpτrss σ1 cos φ cos λ(4.20)pwhere σ1 is the applied tensile stress, φ is the angle between the tensile axisand a vector normal to the plane of interest, and λ is the angle between thetensile axis and the direction of the shear stress. This shear stress has to be inthe plane itself, so for a 2-dimensional sample λ φ 90 . This means we canrewrite Eq. 4.20 in the following way:pτrss σ1 cos φ cos (90 φ)(4.21)We can use the identities cos (90 φ) sin φ and sin (2φ) 2 sin φ cos φ toobtain the following:pτrss σ1sin (2φ)2(4.22)We can get the same thing from the Mohr’s circle construction to redefine thepaxes by a rotation of φ. The shear stress is simply the radius of the circle (φ1 /2in this case) multiplied by sin (2φ). Mohr’s circle also gives us the normalstresses:pσ11 σ22 σ12pσ12p σ12pσ12cos (2φ)(4.23)cos (2φ)The untransformed 2-dimensional stress tensor looks like this: [σ] pσ10 00(4.24)The tra

332: Mechanical Behavior of Materials Department of Materials Science and Engineering Northwestern University April 20, 2022 Contents 1 Catalog Description4 2 Course Outcomes4 . strength, s f, to separate materials on the y axis. When the story begins, all we had to work with are the materials we could find around us or dig out of

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ACI 117 is adopted within the text of ACI 332 Note: Concrete construction in one and two-family dwellings should meet the standards established in ACI 332. Construction means, materials, or methods not addressed in ACI 332 should meet the standards established in ACI 318. Foundation Design: Continuou

Enganche Instrucciones de montaje y de servicio . 332 273 600 001 Nisan Cabstar (406) Renault Maxity. 332 273 691 101 - 007 2 . 332 273 691 101 - 007 3 D sich bitte direkt an Ihren Vertragspar Unsere Produkte werden mit größter Sorgfalt gefertigt.

The Income Tax Act [CAP. 332 R.E 2019] 1 THE UNITED REPUBLIC OF TANZANIA CHAPTER 332 THE INCOME TAX ACT [PRINCIPAL LEGISLATION] REVISED EDITION 2019 This Edition of the Income Tax Act, Cap. 332, has been revised up to and including 30th November, 2019 and is printed under the au

The attached Tables using the ACI 332 table only reference 8" flat wall foundations. ACI 332-14 also has vertical rebar tables for higher strength concrete. Refer to Fox Blocks CAD details 2-01 and 2-02 for reinforcement placement. When utilizing the alternative table R404.1.2(9) or ACI 332 rebar designs ensure

Verbal Behavior Verbal Behavior (V) is a class of behavior that is reinforced through the mediation of other persons (Skinner, 1957, p.2). Verbal Behavior is the application of behavior principles to language. Verbal Behavior categorizes language responses into different categories based on the function of the response Verbal Behavior is a subset of the science of Behavior Analysis

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Am I my Brother’s Keeper? Acts 15:19-35 Introduction: Since the beginning of time when the first man and woman rebelled against God, mankind has been separated from God. Every person since that time has been born into that rebellion and sin. Because of sin, people are separated from God and are unable to have a right relationship with Him or each other. Ill. of evil and suffering Inside of .