MECHANICS OF MATERIALS
11th Edition
ISBN: 9780137605521
Author: HIBBELER
Publisher: RENT PEARS
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Chapter 10.6, Problem 30P
For the case of plane stress, show that Hooke’s law can be written as
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The state of in-plane stress at a point on an element of material is shown. Let |σx| = 370 MPa, |σy| = 130 MPa, and |τxy| = 85.0 MPa. Use this information to represent the state of stress of the same point that is rotated through an angle of θ = 25.0.
For the state of a plane strain with εx, εy and γxy components: (a) construct Mohr’s circle and (b) determine the equivalent in-plane strains for an element oriented at an angle of 30° clockwise. εx = 255 × 10-6 εy = -320 × 10-6 γxy = -165 × 10-6
A tri-axial state of stress, σx , σy, and σz ,exists in a steel machine part. For steel, E = 200GPa and ν = 0.3. Determine the normal strain in the x-direction if σx = 100MPa, σy = 35MPa, σz = 70MPa. Determine the dilatation. Determine the modulus of rigidity.
Chapter 10 Solutions
MECHANICS OF MATERIALS
Ch. 10.3 - Prove that the sum of the normal strains in...Ch. 10.3 - The state of strain at the point on the arm has...Ch. 10.3 - The state of strain at the point on the leaf of...Ch. 10.3 - Use the strain transformation equations and...Ch. 10.3 - Determine the equivalent state of strain on an...Ch. 10.3 - Determine the equivalent state of strain which...Ch. 10.3 - Use the strain transformation equations to...Ch. 10.3 - Determine the equivalent state of strain, which...Ch. 10.3 - Solve Prob.103 using Mohrs circle. 103. The state...Ch. 10.5 - The strain at point A on the bracket has...
Ch. 10.5 - Determine (a) the principal strains at A, (b) the...Ch. 10.6 - For the case of plane stress, show that Hookes law...Ch. 10.6 - to develop the strain tranformation equations....Ch. 10.6 - Determine the associated principal stresses at the...Ch. 10.6 - Determine the applied load P. What is the shear...Ch. 10.6 - If a load of P = 3 kip is applied to the A-36...Ch. 10.7 - A material is subjected to plane stress. Express...Ch. 10.7 - A material is subjected to plane stress. Express...Ch. 10.7 - Solve Prob. 1061 using the maximum distortion...Ch. 10.7 - Solve Prob.1063 using the maximum distortion...Ch. 10.7 - Prob. 70PCh. 10.7 - The plate is made of Tobin bronze, which yields at...Ch. 10.7 - If a machine part is made of titanium (TI-6A1-4V)...Ch. 10.7 - The components of plane stress at a critical point...Ch. 10.7 - If Y = 50 ksi, determine the factor of safety for...Ch. 10.7 - Prob. 82PCh. 10.7 - If the yield stress for steel is Y = 36 ksi,...Ch. 10.7 - Prob. 84PCh. 10.7 - The state of stress acting at a critical point on...Ch. 10.7 - The shaft consists of a solid segment AB and a...Ch. 10 - In the case of plane stress, where the in-plane...Ch. 10 - The plate is made of material having a modulus of...Ch. 10 - If the material is machine steel having a yield...Ch. 10 - Determine if yielding has occurred on the basis of...Ch. 10 - The 60 strain rosette is mounted on a beam. The...Ch. 10 - Use the strain transformation equations to...Ch. 10 - If the strain gages a and b at points give...Ch. 10 - Use the strain-transformation equations and...Ch. 10 - Use the strain transformation equations to...Ch. 10 - Specify the orientation of the corresponding...
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- A thin wire, lying along the x axis, is strained such that each point on the wire is displaced Δx = kx2 along the x axis. If k is constant, what is the normal strain at any point P along the wire?arrow_forwardFour stress elements are shown below. All members have the same value for E (Young’s Modulus) and ν (Poisson’s ratio). Rank the members from largest to smallest absolute value of the normal strain in the y direction.arrow_forwardDetermine the transverse strain in the x axis of the solid subjected to longitudinal tension. 4 cm 1 cm 6x10³ N 2 cm μ = 0,28 E=1,4x10" N/m² 6x10³ Narrow_forward
- Your answer is partially correct. On the free surface of an aluminum [E=10100 ksi; v = 0.35] component, the strain rosette shown was used to obtain the following normal strain data: a=-425 με, ε = -200 με, and ε & εν +575 μɛ. Determine the normal stress that acts along an axis that is rotated at an angle of 0 = 60° counterclockwise from the positive x axis. 60° 60° b a 60° x Determine the normal strains at the point associated with the x and y axes. Answers: Ex = -425 με, ε, Ξ i με.arrow_forwardThe state of stress at a point in a member is shown on the rectangular stress element; the magnitudes of the stresses are |σx|=66 MPa, |σy|=39 MPa|, and |τxy|=71 MPa. Using the stress-transformation equations, determine the state of stress on the inclined plane AB.arrow_forwardThe state of plane strain on an element is represented by the following components: Ex =D340 x 10-6, ɛ, = , yxy Ey =D110 x 10-6, 3D180 x10-6 ху Draw Mohr's circle to represent this state of strain. Use Mohrs circle to obtain the principal strains and principal plane.arrow_forward
- Determine the maximum normal stress on a transverse plane in the straight portion of the structure shown below and clearly indicate where it occurs. The member is braced in the plane perpendicular to the plane of symmetry. Consider (a) Section B-B shown below at the left (symmetric section).(b) Section B-B shown below (unsymmetric).arrow_forwardCan you please explain why the question above is true and if not kindly explain why is False.arrow_forward4. For a state of biaxial strain (ε biax) in a linear-elastic isotropic material, what are the corresponding stresses? How would this change if the Poisson's ratio was zero? Briefly explain why. Assume standard material constants E, v, λ, etc. Γε Ebiax=0 01 bod 000 0 LO 0 0arrow_forward
- 8000 mm3 aluminium cube is stressed in 3 mutually perpendicular direction x,y and z. The stresses in these directions are σx = 50 kPaσy = 80 kPaσz = -100 kPaDetermine the volumetric strain and change in volume. ν is 0.34 and E is 71 GPaarrow_forwardA displacement field in a body is given by u =c(x' +10) v = 2cyz =(-xy+2') w = where c = 104. Determine the state of strain and stress on an element positioned at (0, 2, 1). Use E = 70 GPa and v 0.3.arrow_forwardA 60 ̊ strain rosette measures the following strain at a point on the aluminum skin of an airplane. ε0 = 160 ×10-6 m/m, ε60 = -220 ×10-6 m/m and ε120 = 360 ×10-6 m/m. Using E= 10 ×106 psi and v = 0.3, Determine the principle stresses and the maximum in-plane shear stress.arrow_forward
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