Part AThe stress at a point is shown on the element. Suppose that o, =105 MPа, т - 158 MPаDetermine the principal stress.(Figure 1)Enter your answers numerically using three significant figures separated by commas.VG AEo t vec?Omax, Oint, Omin =MPаSubmitRequest AnswerPart BDetermine the absolute maximum shear stress.Express your answer with three significant figures and use the appropriate units.HAO ) ?Figure1 of 1 >ValueUnitsTimax in-plane =SubmitRequest AnswerProvide Feedback

Part A The stress at a point is shown on the element. Suppose that a = 105 MPa, T,, = 158 MPa . Determine the principal stress. (Figure 1) Enter your answers numerically using three significant figures separated by commas. A AEo vec Omax, Oint, Omin = MPa Submit Request Answer Part B Determine the absolute maximum shear stress. Express your answer with three significant figures and use the appropriate units. HA ? Figure < 1 of 1 Value Units Тmаx in-plane Submit Request Answer

Part A The stress at a point is shown on the element. Suppose that a = 105 MPa, T,, = 158 MPa . Determine the principal stress. (Figure 1) Enter your answers numerically using three significant figures separated by commas. A AEo vec Omax, Oint, Omin = MPa Submit Request Answer Part B Determine the absolute maximum shear stress. Express your answer with three significant figures and use the appropriate units. HA ? Figure < 1 of 1 Value Units Тmаx in-plane Submit Request Answer

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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