8.1 Stress Transformation Method of Equations Choose the best answer in the questions below. The Poisson’s ratio of the material in questions below is 0.25. Name Email 1. The angle to find the normal stress on plane AA in Figure (a) using Equation 8.1 is25 degrees115 degrees65 degrees-25 degreesNone of the above2. The angle to find the normal stress on plane AA in Figure (b) using Equation 8.1 is25 degrees115 degrees65-25 degreesNone of the above3. The angle to find the normal stress on plane AA in Figure (c) using Equation 8.1 is25 degrees115 degrees65 degrees-25 degreesNone of the above4. At a point in plane stress the principal stresses were found to be 22 ksi (T) and 14 ksi (C). The maximum shear stress at the point is11 ksi4 ksi18 ksi6.5 ksiNone of the above5. At a point in plane stress the principal stresses were found to be 22 ksi (T) and 14 ksi (T). The maximum shear stress at the point is11 ksi4 ksi18 ksi6.5 ksiNone of the above6. At a point in plane strain the principal stresses were found to be 22 ksi (T) and 14 ksi (C). The maximum shear stress at the point is11 ksi4 ksi18 ksi6.5 ksiNone of the above7. At a point in plane strain the principal stresses were found to be 22 ksi (T) and 14 ksi (T). The maximum shear stress at the point is11 ksi4 ksi18 ksi6.5 ksiNone of the above8. If the other principal stress was 150 MPa (T) then the principal angle 1 is-35 degrees35 degrees55 degrees-55 degreesNone of the above9. If the other principal stress was 150 MPa (C) then the principal angle 1 is-35 degrees35 degrees55 degrees-55 degreesNone of the above10. If the other principal stress was 75 MPa (T) then the principal angle 1 is-35 degrees35 degrees55 degrees-55 degreesNone of the aboveDo you have any comments or suggestions? Please send them to author@madhuvable.org Time is Up!Time's up