air under a pressure to 16 MPa. The tank has a 180 mm inner diameter and a 12 mm wall thickness (40 points) A torque of magnitude T-24kN-m is applied to the end of a tank containing 3. Part A. Fo...
A torque of magnitude T = 10 kN·m is applied to the end of a tank containing compressed air under a pressure of 8 MPa. Knowing that the tank has a 180-mm inner diameter and a 12-mm wall thickness, determine the maximum normal stress and the maximum shearing stress in the tank. (Round the final answers to one decimal place.) The maximum normal stress in the tank is MPa. The maximum shearing stress in the tank is MPa.
Stress Analysis 3. A 20-mm diameter rod made ofa ductile material with a yield strength of 350 MPa is subjected to torque of 100 N.m and a bending moment of 150 N.m. An axial force is then gradually applied. Determine the value of force when the rod begins to yield. Solve the problem two ways using the (a) Tresca theory (Maximum shearing stress theory) and (b) von Mises theory (Maximum distortion energy theory) [12+12 points 3. A 20-mm diameter rod...
A torque of magnitude 7-9.5 kNm is applied to the end of a tonk containing compressed air under a pressure of 8 MPa Knowing that the tank has a 180-mm inner diameter and a 12-mm wall thickness, determine the maximum normal stress and the maximum shearing stress in the tank. (Round the final answers to one decimal place.) т The maximum normal stress in the tank is MPa The maximum shearing stress in the tank is MPa
Problem 4. A torque of magnitude T = 10 kN·m is applied to the end of a tank containing compressed air under a pressure of 8 MPa. Knowing that the tank has an average diameter of 192-mm and a wall thickness of 12-mm, determine the principal stresses and the maximum shearing stress at some pointed located on the inner surface of the tank. (Note: assume σ, = 0)
The compressed-air tank has an inner radius r and uniform wall thickness t. The gage pressure inside the tank is p and the centric axial load F is applied at the end cap. Use p = 1366 kPa, F = 14 kN, t= 12 mm and r = 192 mm. u x ІН F Matlab Mathematica Python R p = 1366; % kPa F = 14; % KN t = 12; % mm r = 192; % mm sigmay =...
Problem 1. A I meter inner diameter steel pressure tank with 8 mm wall thickness is subject to a internal pressure of 1.5 MPa and due to the piping weight a torsion of 10 Nm is acting as shown in the figure. The length of the cylinder is 3 meters. Determine: The state of stress in the cylinder wall The state of stress if the normal Cartesian system is rotate 250 The principal stress and the principal angle. The maximum...
Problem 1. A 1 meter inner diameter steel pressure tank with 8 mm wall thickness is subject to a internal pressure of 1.5 MPa and due to the piping weight a torsion of 10 N.m is acting as shown in the figure. The length of the cylinder is 3 meters. Determine: The state of stress in the cylinder wall The state of stress if the normal Cartesian system is rotate 25° The principal stress and the principal angle. The maximum...
MEE2001/2015 Q5. A thin walled steel cylinder with 10 mm wall thickness and internal diameter of 200 mm (Fig. Q5) is subjected to an internal pressure, p. The steel used for the cylinder has a yield stress of 240 MPa. +F 200 mm Fig. Q5 (a) If a tensile axial force of 1MN is applied to the end plate, show that the maximum internal pressure that can be applied before the cylinder yields according to the Tresca criterion is 16.2...
Problem 1 A thin-walled pressure vessel of mean radius R 100 mm and thickness t (R) is subjected to cyclic internal pressure p in the range -3 MPa p7 MPa. Using Soderberg's relation with maximum distortional strain energy theory, and safety factor of 2.6 determine the number of cycles to failure ift-5 mm Assume ơy(yield stress)-350 MPa, NY (Number of cycles to yield)-10, ơ (endurance stress)-290 MPa, Ne (number ofcycles associated with endurance stress)-10 Problem 1 A thin-walled pressure vessel...
need solution for milestones A Q1 Solid Mechanics 3 Assessment Task 1a - 2020 Milestone a Question 1. For each of the plane-stress conditions given below, construct a Mohr's circle of stress, find the principal stresses and the orientation of the principal axes relative to the xy axes and determine the stresses on an element, rotated in the x-y plane 60° counterclockwise from its original position: (a) dx = 200 MPa Oy - 300 MPa T .40 MPa (b) dx...