Consider a point in a structural member that is subjected to plane stress. Normal and shear stresses acting on horizontal andvertical planes at the point are shown. Assume stress magnitudes of Sx = 210 MPa, Sxy = 150 MPa.SxyConstruct Mohr's circle for this state of stress on paper and use the results to answer the questions in the subsequent parts of thisGO exercise. For the given state of stress at a point in a structural member, determine the center Cand the radius R of Mohr's circle.Answers: C = iMPa, R = iMPa.Save for LaterSubmit AnswerPart 3Determine the principal stresses (o,1 > Op2 ) for this state of stress.Answers: 0pliMPa, Op2MРа.Save for LaterSubmit AnswerPart 4For this Mohr's circle, determine the magnitude of the central angle between:(a) point x and the point representing the principal stress opi.(b) point x and the point representing the principal stress op2.Answers:(a) Angle = i(b) Angle = iSave for LaterSubmit Answer

Answered: Image /qna-images/answer/79cdff75-ac3a-41a7-9d14-25ab767950db.jpg

Consider a point in a structural member that is subjected to plane stress. Normal and shear stresses acting on horizontal and vertical planes at the point are shown. Assume stress magnitudes of Sy = 210 MPa, Sy = 150 MPa. Sy Construct Mohr's circle for this state of stress on paper and use the results to answer the questions in the subsequent parts of this GO exercise.

Consider a point in a structural member that is subjected to plane stress. Normal and shear stresses acting on horizontal and vertical planes at the point are shown. Assume stress magnitudes of Sy = 210 MPa, Sy = 150 MPa. Sy Construct Mohr's circle for this state of stress on paper and use the results to answer the questions in the subsequent parts of this GO exercise.

Mechanics of Materials (MindTap Course List)

9th Edition

ISBN:9781337093347

Author:Barry J. Goodno, James M. Gere

Publisher:Barry J. Goodno, James M. Gere

Chapter7: Analysis Of Stress And Strain

Section: Chapter Questions

Problem 7.2.8P: An element in plane stress on the fuselage of an airplane (figure part a) is subjected to...

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