Learning Goal: Part A - Orientation of the planes of maximum and minimum normal stress To determine the in-plane principal stresses and maximum shear stress along with their orientations and the average normal stress for an element in a given state of plane stress. Determine the orientation of the planes of maximum and minimum normal stress, 6p1 and ep2, respectively. Use the value f Op2 that is negative. Then use this value to determine the value of Opl. Express your answers to four significant figures separated by a comma. The element of material below is subjected to the state of stress shown, where a = 120.0 MPa, b = 62.00 MPa. and c = 12.00 MPa (Figure 1) • View Available Hint(s) vec ? Opl, Op2 = Submit Figure < 1 of 1 Part B - In-plane principal stresses L, a Determine the in-plane principal stresses for the element (as oriented in Part A), and calculate oj and og such that they correspond with Op1 and O,2. Express answers to four significant figures separated by a comma. > View Available Hint(s) V ΑΣφ It vec 01, o2 = МРа, МРа
Learning Goal: Part A - Orientation of the planes of maximum and minimum normal stress To determine the in-plane principal stresses and maximum shear stress along with their orientations and the average normal stress for an element in a given state of plane stress. Determine the orientation of the planes of maximum and minimum normal stress, 6p1 and ep2, respectively. Use the value f Op2 that is negative. Then use this value to determine the value of Opl. Express your answers to four significant figures separated by a comma. The element of material below is subjected to the state of stress shown, where a = 120.0 MPa, b = 62.00 MPa. and c = 12.00 MPa (Figure 1) • View Available Hint(s) vec ? Opl, Op2 = Submit Figure < 1 of 1 Part B - In-plane principal stresses L, a Determine the in-plane principal stresses for the element (as oriented in Part A), and calculate oj and og such that they correspond with Op1 and O,2. Express answers to four significant figures separated by a comma. > View Available Hint(s) V ΑΣφ It vec 01, o2 = МРа, МРа
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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