A cylindrical specimen of Aluminum having a diameter of 12.8 mm and a gauge length of 50.800 mm is pulled in tension. Use the load-elongation characteristics shown in the following| table to complete Q1(a) through (f). Raw Data Load (N) Length (mm) 50.800 7330 50.851 15100 50.902 23100 50.952 30400 51.003 34400 51.054 38400 51.308 41300 51.816 44800 52.832 46200 53.848 47300 54.864 47500 55.880 46100 56.896 44800 57.658 42600 58.420 36400 59.182 a) Plot both the engineering stress versus engineering strain and true stress versus true strain curves on the same axis. b) Compute the modulus of elasticity. c) Determine the yield strength at a strain offset of 0.002. d) Determine the tensile strength of this alloy. e) Compute the modulus of resilience. f) What is the ductility, in percent elongation?

In the figure shown, the rigid beam with negligible mass was horizontal before the load P was applied. Determine the value of load P if the vertical movement at P is 3mm. Draw the FBD and deformation diagram.

The overhead beam in the figure has the composite section given below. The bending moment vector acts at an angle of 0-60 degrees with the horizontal z-axis of the beam section as shown in the figure. Determine the stress at point K of the beam section for the maximum bending moment under the forces acting on the beam. Note: The numerical values of the relevant parameters are given in the attached table for each student. K Z< M 0 40mm 395 mm B2 40mm B1 240 mm + 45 mm H 180 mm 45 mm 32 KN -1.6 m B 2.4 m с 36 kN/m 6.4 m D

Given: E= 29x10^6 psi A= 2in^2 Determine the deformations members AB, BC, BE, DE and DF. Please show your complete handwritten solution.

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It is the same as my question before. Please see the image attached. Please also check my previous questions.Thank you and God bless

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The adjacent sketch indicates a brass wire which is exactly 12.00 m long and a steel wire which is 12.01 m long. Each wire has a cross-sectional area of 150 mm2 . What load does each wire carry if E steel = 200,000 MPa & E brass = 110,000 MPa? (Hint: no load on steel wire until brass wire stretches by 10mm, then ratio of stresses in each wire is same as ratio of E v

A stat of stress is specified in Figure. By using Mohr's circle determine the normal and shearing stresses on (a) the principal planes, (b) the planes of maximum shearing stress. 20 MPa 32 MPa 10 MPa 10 MPa 32 MPa 20 MPa I need a clear answer by hand, not by keyboard and fast answer within 20 minutes. Thank you | dybala

i need the answer quickly