Strain Transformation Lecture 4-b Mechanics of Materials (Chapter 10) By R. C. Hibbeler Course: Strength of Materials-II Instructor: Dr. Shahzad Saleem Department of Civil Engineering University of Engineering and Technology, Taxila 1 Strength of Materials-II University of Engineering and Technology, Taxila 10.3 Mohr’s Circle—Plane Strain 2 Strength of Materials-II University of Engineering and Technology, Taxila 10.3 Mohr’s Circle—Plane Strain Since the equations of plane-strain transformation are mathematically similar to the equations of plane-stress transformation, we can also solve problems involving the transformation of strain using Mohr’s circle. Like the case for stress, the parameter θ in Eqs. 10–5 and 10–6 can be eliminated and the result rewritten in the form 3 Strength of Materials-II University of Engineering and Technology, Taxila 10.3 Mohr’s Circle—Plane Strain Equation 10–13 represents the equation of Mohr’s circle for strain. It has a center on the ϵ axis at point C(ϵavg, 0) and a radius R. Notice how these equations compare with Eqs. 9–11 and 9–12. Here ϵx', ϵavg, and γxy/2 replace σx', σavg, and τxy. 4 Strength of Materials-II University of Engineering and Technology, Taxila 10.3 Mohr’s Circle—Plane Strain Procedure for Analysis 5 Strength of Materials-II University of Engineering and Technology, Taxila 10.3 Mohr’s Circle—Plane Strain Principal Strains 6 Strength of Materials-II University of Engineering and Technology, Taxila 10.3 Mohr’s Circle—Plane Strain Maximum In-Plane Shear Strain 7 Strength of Materials-II University of Engineering and Technology, Taxila 10.3 Mohr’s Circle—Plane Strain Strains on Arbitrary Plane 8 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.4 9 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.4 The state of plane strain at a point is represented by the components ϵx = 250(10-6), ϵy = -150(10-6), and γxy = 120(10-6). Determine the principal strains and the orientation of the element. SOLUTION: Construction of the Circle The center of the circle C is located on the ϵ axis at 10 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.4 SOLUTION: Construction of the Circle Since γxy/2 = 60(10-6), the reference point A (θ = 0°) has coordinates A(250(10-6), 60(10-6)). From the shaded triangle in Fig. 10–10a, the radius of the circle is CA ; that is, 11 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.4 SOLUTION: Principal Strains The ϵ coordinates of points B and D represent the principal strains. They are The direction of the positive principal strain ϵ1 is defined by the counterclockwise angle 2θp1, measured from the radial reference line CA (θ = 0°) to the line CB. We have 12 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.4 SOLUTION: Principal Strains 13 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.5 14 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.5 The state of plane strain at a point is represented by the components ϵx = 250(10-6), ϵy = -150(10-6), and γxy = 120(10-6). Determine the maximum inplane shear strains and the orientation of the element. SOLUTION: Construction of the Circle The circle has been established in the previous example. 15 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.4 SOLUTION: Maximum In-Plane Shear Strain Half the maximum in-plane shear strain and average normal strain are represented by the coordinates of point E or F on the circle. From the coordinates of point E, 16 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.4 Maximum In-Plane Shear Strain To orient the element, we can determine the clockwise angle 2θs1 measured from CA (θ = 0°) to CE. 17 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.6 18 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.6 The state of plane strain at a point is represented by the components ϵx = 300(10-6), ϵy = -100(10-6), and γxy = 100(10-6). Determine the state of strain on an element oriented 20° clockwise from this reported position. SOLUTION: Construction of the Circle The ϵ and γ/2 axes are established in Fig. 10–12a. The center of the circle is on the ϵ axis at 19 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.6 Construction of the Circle The reference point A has coordinates A(-300(10-6), 50(10-6)). The radius CA determined from the shaded triangle is therefore 20 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.6 Strains on Inclined Element Since the element is to be oriented 20° clockwise, we must establish a radial line CP, 2(20°) = 40° clockwise, measured from CA (θ = 0°), Fig. 10– 12a. The coordinates of point P (ϵx', γx'y'/2) are obtained from the geometry of the circle. 21 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.6 Strains on Inclined Element Since the element is to be oriented 20° clockwise, we must establish a radial line CP, 2(20°) = 40° clockwise, measured from CA (θ = 0°), Fig. 10– 12a. The coordinates of point P (ϵx', γx'y'/2) are obtained from the geometry of the circle. 22 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.6 Strains on Inclined Element The normal strain ϵy' can be determined from the ϵ coordinate of point Q on the circle, Fig. 10–12a. 23 Strength of Materials-II University of Engineering and Technology, Taxila 10.4 Absolute Maximum Shear Strain 24 Strength of Materials-II University of Engineering and Technology, Taxila 10.4 Absolute Maximum Shear Strain In Sec. 9–5 it was pointed out that in the case of plane stress, the absolute maximum shear stress in an element of material will occur out of the plane when the principal stresses have the same sign, i.e., both are tensile or both are compressive. A similar result occurs for plane strain. For example, if the principal in-plane strains cause elongations, Fig. 10–13a, then the three Mohr’s circles describing the normal and shear strain components for elements oriented about the x', y', and z' axes are shown in Fig. 10–13b. 25 Strength of Materials-II University of Engineering and Technology, Taxila 10.4 Absolute Maximum Shear Strain By inspection, the largest circle has a radius R = (γx'z') max /2. Hence, This value gives the absolute maximum shear strain for the material. Note that it is larger than the maximum in-plane shear strain, which is (γx'y')max = ϵ1 - ϵ2. 26 Strength of Materials-II University of Engineering and Technology, Taxila 10.4 Absolute Maximum Shear Strain Now consider the case where one of the in-plane principal strains is of opposite sign to the other in-plane principal strain, so that ϵ1 causes elongation and ϵ2 causes contraction, Fig. 10–14a. Mohr’s circles, which describe the strains on each element’s orientation about the x', y', z' axes, are shown in Fig. 10–14b. Here 27 Strength of Materials-II University of Engineering and Technology, Taxila 10.4 Absolute Maximum Shear Strain We may therefore summarize the above two cases as follows. If the in-plane principal strains both have the same sign, the absolute maximum shear strain will occur out of plane and has a value of γmaxabs = ϵmax. However, if the in-plane principal strains are of opposite signs, then the absolute maximum shear strain equals the maximum in-plane shear strain. 28 Strength of Materials-II University of Engineering and Technology, Taxila 10.4 Absolute Maximum Shear Strain 29 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.7 30 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.7 The state of plane strain at a point is represented by the strain components ϵx = -400(10-6), ϵy = 200(10-6), and γxy = 150(10-6). Determine the maximum in-plane shear strain and the absolute maximum shear strain. SOLUTION: Maximum In-Plane Shear Strain From the strain components, the center of the circle is on the ϵ axis at 31 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.7 SOLUTION: Maximum In-Plane Shear Strain Since γxy/2 = 75(10-6), the reference point A has coordinates (-400(10-6), 75(10-6)). As shown in Fig. 10–15, the radius of the circle is therefore 32 Strength of Materials-II University of Engineering and Technology, Taxila Example 10.7 SOLUTION: Absolute Maximum Shear Strain From the above results, we have ϵ1 = 209(10-6), ϵ2 = -409(10-6). The three Mohr’s circles, plotted for element orientations about each of the x, y, z axes, are also shown in Fig. 10–15. It is seen that since the principal inplane strains have opposite signs, the maximum in-plane shear strain is also the absolute maximum shear strain; i.e., 33