16 ksi (T), Gy= 13 ksi (T), o. = 11ksi (T), T,y = 4 ksi, T = -4 ksi,Ata point in a stressed body, the known stresses are o, =and T = 0.Determine(a) the normal and shear stresses on a plane whose outward normal is oriented at angles of 42° 58°, and 65.89° with thex, y, and zaxes, respectively.(b) the principal stresses and the absolute maximum shear stress at the point.Determine the three orthogonal components of the resultant stress.Answers:Sx =ksiSy=ksiSz =ksi

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Ata point in a stressed body, the known stresses are o, = and T = 0, Determine a) the normal and shear stresses on a plane whose outward normal is oriented at angles of 42°, 58°, and 65.89° with the x, y, am exes, respectively. b) the principal stresses and the absolute maximum shear stress at the point. Determine the three orthogonal components of the resultant stress. Answers: Sx= ksi Sy= ksi ksi

Ata point in a stressed body, the known stresses are o, = and T = 0, Determine a) the normal and shear stresses on a plane whose outward normal is oriented at angles of 42°, 58°, and 65.89° with the x, y, am exes, respectively. b) the principal stresses and the absolute maximum shear stress at the point. Determine the three orthogonal components of the resultant stress. Answers: Sx= ksi Sy= ksi ksi

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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