A vertical rod of elastic material is fixed at both ends with constant cross-sectional area A, Young’s modulus E, and height of L under the distributed load f per unit length. The vertical deflection
Using three elements of equal length, solve for
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- B A 10 kN/m 3 m 20 kN 10 m 3 m C 丬 D Use the method of superposition to solve the following problems and assume that the flexural rigidity E/ of each beam is constant.arrow_forwardضحقهكشتبhelparrow_forwardArrangement of the solution: The following section should be underlined and numbered in your solution Problem statement Given Required Drawing/ sketch / free body diagram V. Solution with explanationarrow_forward
- A 50-mm diameter cylinder is made of a brass for which the stress-strain diagram is as shown. The angle of twist is 5° in a length L = 725 mm. The three points on the nonlinear stress-strain diagram used are (0, 0), (0.0015, 55 MPa), and (0.003, 80 MPa). By fitting the polynomial T = A + By + Cy² through these points, the following approximate relation has been obtained. T= 46.7 × 10%y-6.67 × 1012/2 Determine the magnitude Tof torque applied to the shaft using this relation and the two equations given below. Y Ty - ρφ T (MPa) 2π ζ ρ?τὰρ 100 80 60 40 20 0 0.001 0.002 0.003 Y d = 50 mm L The magnitude T of torque applied to the shaft is kN.m.arrow_forwardA 50-mm diameter cylinder is made of a brass for which the stress-strain diagram is as shown. The angle of twist is 5° in a length L = 845 mm. The three points on the nonlinear stress-strain diagram used are (0, 0), (0.0015, 55 MPa), and (0.003, 80 MPa). By fitting the polynomial T = A + By+ Cy2 through these points, the following approximate relation has been obtained. T= 46.7 x 10y-6.67 × 10122 Determine the magnitude T of torque applied to the shaft using this relation and the two equations given below. P4 Y = Ty = 2π] ρ?τὰρ 7 (MPa) 100 80 60 40 20 0 0,001 0.002 0.003 Y d = 50 mm "K The magnitude T of torque applied to the shaft is KN-m. A²arrow_forwardQuestion 4 Consider a thin rectangular cantilever beam of linear elastic and isotropic material in Figure 2. The solution to this two dimensional plane stress problem under point load, F and moment, M is obtained from the Airy's stress function as: i. ii. Φ y M 40313. F Figure 2 ——▬▬▬▬▬▬▬▬▬▬ y² Determine the stress components. Using boundary conditions, investigate how the load F and M are applied to the beam to satisfy the given Airy function. 4c X OL 2c t=1arrow_forward
- 0.0107 0.0043 0.0021 Let D= 0.0043 0.0085 0.0043 be a flexibility matrix, with flexibility measured in inches per pound. Suppose that forces of 40, 20, and 50 lb are applied to a beam at points 1, 2, and 3, respectively. Find the corresponding 0.0021 0.0043 0.0107 deflections y1. y2, and y3- #1 y1 = inch(es) (Round to the nearest thousandth as needed.)arrow_forwardAnalyse the statically determinate bar illustrated below by expressing the loading as a single function using Macaulay brackets and the Dirac delta, integrating to find th axial force and integrating again to find the displacements, applying the boundary conditions appropriately. Find the axial force in the bar at point A and the displaceme at point B. The cross section of the bar is constant with EA = 18000 kN. a = 4 m, b = 2 m, c = 2 m and d = 4 m. w1 = 12 kN/m, w2 = 17 kN/m,, P1 = 12 kN and P2 = 19kN. a W1 L/2 W2 Multiple Choice Answers Multiple Choice Answer: Axial force at point A (kN, tension positive): a. 3.31 b. 31.97 c. 37.33 d. 31 Multiple Choice Answer: Displacement at point B (mm, positive to right): a. 0.0061 b. 0.0395 c. 0.0193 d. 0.0261 Axial force at point A (kN, tension positive): Displacement at point B (mm, positive to right): L/2 P1 P2 (type in your multiple choice answer, e.g. a, b, c or d) (type in your multiple choice answer, e.g. a, b, c or d)arrow_forwardIn mechanical resistancearrow_forward
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