You need the shear modulus for a particular material in order to calculate shear strain for a known applied shear shear stress. You can't find shear modulus for the material, but you can find elastic modulus (200 GPa) and Poisson's ratio (0.3). Which of the following could you use as the shear moduluc for vour calculations2

You need the shear modulus for a particular material in order to calculate shear strain for a known applied shear shear stress. You can't find shear modulus for the material, but you can find elastic modulus (200 GPa) and Poisson's ratio (0.3). Which of the following could you use as the shear moduluc for vour calculations2

Mechanics of Materials (MindTap Course List)

9th Edition

ISBN:9781337093347

Author:Barry J. Goodno, James M. Gere

Publisher:Barry J. Goodno, James M. Gere

Chapter7: Analysis Of Stress And Strain

Section: Chapter Questions

Problem 7.7.19P: During a test of an airplane wing, the strain gage readings from a 45° rosette (see figure) are as...

See similar textbooks

Similar questions

The stress-strain curves of materials A, B and C are given in Figure. Answer the questions according to curves. a. Stress (MPa) C. 1400 1200 1000 Stress (MPa) 800 600 400 200 0 0.po 1200 1000 800 600 400 200 O 0.000 0.002 0.004 0.006 0.008 0.10 Strain 0.010 Strain Rank the materials from most ductile to most brittle. 0.15 0.012 0.014 Calculate the modulus of elasticity in GPa of each material 0.20 с b. Determine the tensile strength of each material. Show your work on the stress-strain curve. 0.016 0.018 0.020
Given a stress state of ø, = -4 MPa, øy = 12 MPa, ty = 7 MPa ccw 1) Draw a properly oriented stress element illustrating this state of stress 2) Using Mohr's circle, find the principal stresses and directions, and show these on a stress element correctly aligned with respect to the xy coordinates. Draw another stress element to show zi and 72, find the corresponding normal stresses, and label the drawing completely. 3) Use the plane-stress transformation equations to validate your answers in part 2
Please complete the solution to be similar to the most important line. It's the same line I uploaded a picture of you
1.6-7 A wire of length L = 2.5 m and diameter d = 1.6 mm is stretched by tensile forces P = 600 N. The wire is made of a copper alloy having a stress- strain relationship that may be described mathemat- ically by 124,020ɛ 0 s8s 0.03 (o = MPa) 1+ 300ɛ in which e is nondimensional and o has units of MPa. (a) Construct a stress-strain diagram for the material. (b) Determine the elongation of the wire due to the forces P. (c) If the forces are removed, what is the permanent set of the bar? (d) If the forces are applied again, what is the proportional limit?
Please give a detailed solution in a handwritten format . Use FBD to explain
why the expert here wrote -200 cos 75 when Σ Fx = 0 , I understand all steps but how he got - 200 cos 75 ( for the force ) (how the angle is 75 ) can you please clarify for me this point please ...... because I did not got the angle 75 dgree for 200 N force can you draw a diagrm for me please to see how 75 dgree links to 200 N
Answer the problem with detailed step by step solution refer to the table of equations when answering the problem.
Find the force pneed to fill the gap. Young's modulus as 300 GPa C 1,5 cm² 2 cm2 P. A 1 cm 1/2 p 0.5 m 0.5 m 1 m 0.5 mm (a) 13.84KN. (b) 14.21KN.
The plane stress displacement field for the pure bending problem was given by u = - El v = (vy? + x² - P), where -1
Don't copy ,Please provide Diagram and Equation as a part of explanation with correct Final answer. [ Try within 30-45minutes]
The flow stress (in MPa) of a material is given by o = 500 0.1, Where & is true strain. The Young's modulus of elasticity of the mater 41 is 200GPa. A block or thickness 100 mm made of this material is compressed to 95 mm thickness and then the load is removed. The final dimension of the block (in mm) is
Last 2