Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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- Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizontal and vertical planes at the point are Sx= 14 MPa, S, = 29 MPa, and Sy = 39 MPa. (a) Determine the principal stresses (o,1 > op2) and the maximum in-plane shear stress Tmax acting at the point. (b) Find the smallest rotation angle 0, (counterclockwise is positive, clockwise is negative) that will rotate to principal directions. Then show these stresses in an appropriate sketch (e.g., see Figure 12.15 or Figure 12.16) Sy Answers: Opl = i MPa. Op2 = i MPa. Tmax = i MPa. Op iarrow_forwardThis is Mechanical Engineering. Please answer with clear work and answers. Thank youarrow_forwardThe strain rosette shown was used to obtain normal strain data at a point on the free surface of a machine component. Given the values = -165 µμe, e = -155 μe, e = 50 μe, E = 10,600 ksi, and v=0.33, determine (a) the stress components o,,o,, and ry at the point. (b) the principal stresses and the maximum in-plane shear stress at the point; on paper, show these stresses on an appropriate sketch that indicates the orientation of the principal planes and the planes of maximum in-plane shear stress. (c) the magnitude of the absolute maximum shear stress at the point. 45° 45°arrow_forward
- The same circular plate, as in the previous questions, is considered. Assume a plate radius of Ro=490mm and a plate thickness of h=9.64mm, respectively. Also, assume that the plate is subjected to a uniform pressure of P=1,440 KPa, and that the plate is made of a material of Poisson's ratio V=0.34. Find the absolute value of the radial stress at the centre of the plate in KPa. NOTES: type in your answer without considering any negative sign; round-off your answer to 4 decimal places. ↓ r> P Ro VITarrow_forwardThe diagram below shows Mohr’s circle for a point in a physicalobject that is subjected to plane stress.(a) Determine the stresses σ x, σ y, and τ xy, and show them on astress element.(b) Determine the principal stresses and the maximum in-planeshear stress acting at the point, and show these stresses on anappropriate sketcharrow_forwardDetermine the average normal stress developed at points A, B, and C: 0.5in ● A TP₂ Iin. ↓ ● B 0.5in ● P3 ↑ C P4 P₁ ↑ The diameter of each Segment is indicated in the figure above. Take P₁ = 3 kip, P2 = 9 kip, P3 = 8 kip, P4 = 2 kiparrow_forward
- answer this ; The von Mises equivalent stresses at point H can be calculated as MPaarrow_forwardDetermine the principal stresses at points A and B of the cylinder. Consider: L = 70 mm; d = 20 mm; F = 12 kN; P = 15 kN; T = 800 Nm.arrow_forwardA 60 ̊ strain rosette measures the following strain at a point on the aluminum skin of an airplane. ε0 = 160 ×10-6 m/m, ε60 = -220 ×10-6 m/m and ε120 = 360 ×10-6 m/m. Using E= 10 ×106 psi and v = 0.3, Determine the principle stresses and the maximum in-plane shear stress.arrow_forward
- Mohr’s circle is shown for a point in a physical object that is subjected to plane stress. Each grid square is 16 MPa in size. (a) Determine the stresses σx, σy, and the magnitude of τxy and show them on a stress element. (b) Determine the stresses σn, σt, and the magnitude of τnt and show them on a stress element that is properly rotated with respect to the x-y element. The sketch must include the magnitude of the angle between the x and n axes and an indication of the rotation direction (i.e., either clockwise or counterclockwise).arrow_forwardAt room temperature (20°C), a 0.5-mm gap exists between the ends of the rods shown. The temperature eventually reaches a value of 140°C. Determine the normal stress in the aluminum rod. Determine the change in length of the aluminum rod.arrow_forwardA state of stress at a point A is given by σx = -75 MPa, σy = 122 MPa, and τxy = -3.75 MPa. Which of the following is one of the principal stresses for the point A.arrow_forward
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