Please give detailed explanation. see photo for expected answer.For the following data, using the stress-transformation equations. (a) find the principal stresses and show their sense on properly oriented elements;(b) find the maximum (principal) shear stresses with the associated normal stresses and show the results on properly oriented elements; and(c) check theinvariance of the normal stresses for solutions in (a) and (b).Please give detailed explanation. See photo for expected answer. 11-202025-10(a) 0, = 5+ (is+20)=30 MPaO2 = 5-25 - -20 MPa(b; Tmax = 25MPA , 6 = 5 MPa(c) G, + 6z = 10 = Ox+ bg 1-17 through 11-20. For the following data, using the stress-transformationcquations, (a) find the principal stresses and show their sense on properly orientedclements: (b) find the maximum (principal) shear stresses with the associated nor-mal stresses and show the results on properly oriented elements:; and (e) check theinvariance of the normal stresses for solutions in (a) and (b).20 -20)11-20.MPa-20 -10,

1-17 through 11-20. For the following data, using the stress-transformation cquations, (a) find the principal stresses and show their sense on properly oriented elements: (b) find the maximum (principal) shear stresses with the associated nor- mal stresses and show the results on properly oriented elements; and (c) check the invariance of the normal stresses for solutions in (a) and (b).

1-17 through 11-20. For the following data, using the stress-transformation cquations, (a) find the principal stresses and show their sense on properly oriented elements: (b) find the maximum (principal) shear stresses with the associated nor- mal stresses and show the results on properly oriented elements; and (c) check the invariance of the normal stresses for solutions in (a) and (b).

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 7.7.19P: During a test of an airplane wing, the strain gage readings from a 45° rosette (see figure) are as...

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