The state of stress at a point in a member is shown on the element as in Figure A4. Determine; i. The stress components acting on the plane AB. ii. The principal stresses and its orientations. i. The maximum shear stress and the absolute maximum shear stress. iv. Sketch all the result on the element and their orientations. 28 MPa 50 MPa 100 MPa Figure A4 ANILAH KALA

The state of stress at a point in a member is shown on the element as in Figure A4. Determine; i. The stress components acting on the plane AB. ii. The principal stresses and its orientations. i. The maximum shear stress and the absolute maximum shear stress. iv. Sketch all the result on the element and their orientations. 28 MPa 50 MPa 100 MPa Figure A4 ANILAH KALA

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

Find the Normal Stress at points A, B, and C in the Rod below. Dimensions given are diameters.
Considering the original state of stress as shown in figure below and recalling the already developed equations for normal and shear stress at an angle Ɵ c.c.w from x-axis, mathematically prove that the planes of maximum in-plane shear stress are inclined at 45o to the principal planes.
Please solve all. Both Questions Please.
A state of plane stress is illustrated in the stress element in Figure 3. (a) (b) 30 MPa Figure 3. 40 MPa 60 MPa y X Find the center, X and Y of the Mohr circle. Plot the Mohr circle using these points. From the Mohr circle, find the principal stress and the maximum shear stress. Indicate on the Mohr circle where these values are found.
use angle of 92 please
In a stressed element, the value of normal stress along 'X' and 'Y' directions are 100 MPa (tensile) and 50 MPa (tensile) respectively and no shear stress is acting on the plane. Find the Normal stress, if the position of principal plane is 0 to major axis. The normal stress in MPa =
In a stressed element, the value of normal stress along 'X' and 'Y' directions are 250 MPa (tensile) and 125 MPa (tensile) respectively and no shear stress is acting on the plane. Find the Normal stress, if the position of principal plane is 0° to major axis. The normal stress in MPa =
At a point of a material, the stresses forming a two-dimensional system are shown inFigure Q1. By using Mohr's circle of stress method: -(i) determine the magnitudes of the principal stresses.(ii) determine the directions of the principal stresses.(iii) Examine the value of the maximum shearing stress.
The state of stress shown to the left was produced by a combination of loadings on a body that is not shown. Determine the following via Mohr's circle: A) Draw Mohr's Circle for the x-y plane. B) Determine the principal stresses - All 3. C) Sketch a properly oriented differential element showing the principal stresses in the x-y plane. D) Determine the magnitude of the maximum shear stress in the x-y plane. E) Sketch a properly oriented differential element showing the maximum shear stress state in the x-y plane. F) Determine the magnitude of the absolute maximum shear stress (and include the two out of plane circles on your original figure). Use the following values for the magnitudes of the stresses: x = 0₂ Txy Ox X X 10 ksi, σy = 4 ksi, σ₂ = 3 ksi, Txy = 4 ksi
a. What is the stress in MPa at point B? b. What type of stress "at point B"
Please use a handwritten solution
Q-1 Figure Q-1, below, shows Mohr’s circle for a point in a physical object that is subjected to plane stress. Determine the stresses σx, σy, and τxy, and show them on a stress element, properly oriented with reference to x-y axes. Determine the principal stresses σ1, σ2, and τmax and show them on a stress element properly rotated with respect to the x–y element Determine the stresses σn, σt, and τnt, and show them on a stress element that is properly rotated with respect to the x–y The sketches must include the magnitude of the angles w.r.t. positive x-axis as well as the angle between the x and n axes, and an indication of the direction of rotations (i.e., either clockwise (c.w.) or counterclockwise (c.c.w.)).