The state of plane stress at a point is shown in Figure 1. By using the Stress Transformation Formula, calculate: i) The principal stresses, and their locations. ii) The maximum in-plane shearing stresses and their locations. iii) The normal and shear stresses on a plane make an angle of *4A°. *A is sum (total) of your ID No. (until become a single digit) *If odd numbers (assume the angle is clockwise) *If even numbers (assume the angle is counter-clockwise) iv) Check your answers in (i), (ii), and (iii) by using Mohr's Circle Method. Show all the values on the graph paper. All the principal values must be clearly written on graph paper. vo MD.

The state of plane stress at a point is shown in Figure 1. By using the Stress Transformation Formula, calculate: i) The principal stresses, and their locations. ii) The maximum in-plane shearing stresses and their locations. iii) The normal and shear stresses on a plane make an angle of 4A°. A is sum (total) of your ID No. (until become a single digit) If odd numbers (assume the angle is clockwise) If even numbers (assume the angle is counter-clockwise) iv) Check your answers in (i), (ii), and (iii) by using Mohr's Circle Method. Show all the values on the graph paper. All the principal values must be clearly written on graph paper. vo MD.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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