Determine the maximum stress produced by the loads and create the shear and moment diagrams for the following: 6-48Introduction to Finite Element AnalysisExercisesDetermine the maximum stress produced by the loads and create the shear and momentdiagram.1. Material: Steel; Diameter 2.5 in. taleFixed end2. Material: AluminumCross section50 lb2 ft.2 ft.6 ft.30 lb/ft

Answered: 6-48 Introduction to Finite Element…

Elements Of Electromagnetics

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ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

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2-8 The stress-strain data from a tensile test on a cast-iron specimen are Engineering stress, MPa 35 70 112 133 182 224 280 332 343 378 5.0 Engineering strain, e • 10 mm/mm 0.20 0.44 0.80 1.0 1.5 2.0 2.8 3.4 4.0 Plot the stress-strain locus and find the 0.1 percent offset yield strength, and the tangent mod- ulus of elasticity at zero stress and at 140 MPa.
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Downloads/ * Practice problem 2 Determine the location of the shear centre O of the thin-walled member of uniform thickness having the cross-section shown. [Ans. 5a/7] UNIVERSITY OF LIVERPOOL $ 4 € R LL F % 5 T G 40 6 Y & O. 7 T Second moment of area liyi U E H J 2a 8 S B K O O L P [ = www.check-p www.check-plag This site was upc via Microsoft Edge delete backspace #
The internal loadings at a section of the beam in (Eigure 1) are shown Figure 20 mm 100 mm 200 mm 20 mm 10 kNm 20 mm 10/12 60 kN 80 KN 500 N-m Determine the in-plane principal stresses at point C. Also compute the maximum in-plane shear stress at this point Express your answers, separated by commas, to three significant figures. VAZ Ivec 4 d Submit Provide Feedback T Wha Bequest Answer ? MPA, MPA, MPA
The thin-walled open cross section shown is transmitting torque 7. The angle of twist ₁ per unit length of each leg can be determined separately using the equation 01 = 3Ti GLIC 3 where G is the shear modulus, ₁ is the angle of twist per unit length, T is torque, and L is the length of the median line. In this case, i = 1, 2, 3, and T; represents the torque in leg i. Assuming that the angle of twist per unit length for each leg is the same, show that T= Lic³ and Tmaz = G01 Cmax Consider a steel section with Tallow = 12.40 kpsi. C1 2 mm L1 20 mm C2 3 mm L2 30 mm C3 2 mm L3 25 mm Determine the torque transmitted by each leg and the torque transmitted by the entire section. The torque transmitted by the first leg is | N-m. The torque transmitted by the second leg is N-m. The torque transmitted by the third leg is N-m. The torque transmitted by the entire section is N-m.
3) Solve the plane stress problem using two-element model to find displacements and stresses. 15 kN 30 mm E-70 GPa Thickness - 10 mm
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Use the graphical method to construct the shear-force diagram and identify the magnitude of the largest shear force (consider both positive and negative). The ground reactions at the wall of the cantilever are provided. L₁= 14.75 ft L₂ = 7.75 ft Vc = 91.50 kips Mc = 706.4375 kip-ft 20 kips 6 kips/ft L₁ 103.50 kips 68.50 kips 91.50 kips O 79.50 kips O 114.50 kips 70 kips BO 12 kips/ft L2 O Vc Mc
A circular pipe of internal diameter 30 mm and thickness 4 mm is subjected to a force 30 kN and the elongation was measured as 1 mm. If the length of the pipe is 2 m, find the value of Young's modulus of elasticity and the stress in the pipe. Match each item to a choice: Young's Modulus (GPa) Stress (MPa): Choices: : 140.4 # 47.9 B 56.4 # 120.8 #240.8 8 70.2
Problem 7: Non-circular cross section shaft related to torque problems are difficult to be solved using the basic theory as for circular shaft. Your role is to make use of FAE to analyze the stress in squared cross section shaft shown in Figure.5. g= 6.5(10%) N/cm? e = 0.035 deg 0.5 cm 0.5 cm 0.5 cm- 0.5 cm Figure.5: Squared cross section shaft applied to torque T as 3D model Provide justified explanation and recommendations to simplify the problem from three-dimensional (3D) to two- dimensional (2D). b. а. If the governing boundary value problem equation of such a problem can be given by: + 2g0 = 0, dy? $(x,y) at boundary is 0 dx2
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6-48 Introduction to Finite Element Analysis Exercises Determine the maximum stress produced by the loads and create the shear and moment diagram. 1. Material: Steel; Diameter 2.5 in. tale Fixed end 2. Material: Aluminum Cross section 50 lb 2 ft. 2 ft. 6 ft. 30 lb/ft