Machine Design Problem
Please show all work and steps
Machine Design Problem Please show all work and steps For the stress states shown, find the...
please write the steps clearly 1. For each stress states listed below, 1) Calculate all three principal stresses and max shear stress 2) Draw a 3D Mohr's circle diagram (a) 0. - 30 MPa, y =-60 MPa, Twy - 30 MPa cw (b) 0,= -40 MPa, 0, = 10 MPa, Twy - 15 MPa CCW (a) 0, 20 kpsi, 0, 0 kpsi, o, - 20 kpsi, ty = 40 kpsi, T -2072 kpsi, and T 0 kpsi
PLEASE SHOW ALL STEPS! 4. The stress element on the fuselage of an airplane shown below is Gx 400 MPa; Oy -300 MPa; and Txy 200 MPa (clockwise). a. Draw the initial stress element showing the stresses acting on it. b. Showing your X and Y coordinate points clearly, draw the complete Mohr's circle on the attached graphing paper From the Mohr's circle, determine Gmax, Omin, and Tmax c. d. Draw the complete principal stress element. Draw the maximum shear...
The block diagrams below show states of stress on soil elements. For each state of stress, perform the following tasks: 1. Sketch a Mohr circle of stress 2. Identify the major and minor principal stresses, σ1 and σ3, and the maximum shear stress, τmax 3. Compute the mean stress and shear stress invariants, p and q. Note that p = 1⁄2(σ1+ σ3) and q = σ1-σ3 for two-dimensional stress conditions where we ignore the intermediate principal stress, σ2. 4. Identify...
Please show all work! Thank you! Determine the equivalent state of stress on an element at the point which represents the principal stresses and the maximum in-plane shear stress and the associated average normal stress. Also, for each case, determine the corresponding orientation of the element with respect to the element shown in the figure below. Solve the problem using Mohr's circle. (Figure 1) Part D Determine the shear stress Try that acts on the element with orientation 0 =...
Please use the numbers provided in the problem statement. Also, if you could show all formulas/equations used that would be great! Thank you so very much! Please use the numbers provided in the problem statement. Also, if you could show all formulas used that would be great! Thank you so very much! For vertical flexural member BD, determine the principal stresses o, i > ?p2) and the maximum shear stress ? as acting at point H as shown. Show these...
please help asap and please show all work. thank you! table 1 data for 7075-T6 below table 2 data for 7075-T6 below i added the tables. they correspond within the pictures 2) Using data from Table A.1 and A.2, for Aluminum 7075-T6, for given a stress amplitude d+460 MPa a. What are the ELASTIC strain amplitude and the PLASTIC strain amplitude? b. What is the TOTAL strain amplitude? c. Draw accurately to scale, the o-e hysteresis loop for this load...
Please show all the steps and calculations, thanks PROBLEM 1 The rolled-steel beam shown has been reinforced by attaching to it two 10 x 175-mm plates, using 20-mm-diameter bolts spaced longitudinally every 150 mm. Knowing that the average allowable shearing stress in the bolts is 90 MPa, determine the largest permissible vertical shearing force. W250 x 44.8