Part C-Maximum deflection What is the maximum deflection of the beam? Express your answer in terms of E, I, w, and L. ► View Available Hint(s) Umax = 197| ΑΣΦ ↓↑ vec ?
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Parts A and B have already been answered, please find vmax
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- The beam ABC made of steel is receiving a point load P at the right end C. Please solve two problems from d to e. (a) Find the reaction from the supports A and B.(b) Use the double integration method to express the deflection y for the beam AB part as an equation for x (including E, I, P, a, L).(c) And use the following values to express the maximum value ymax of the deflection at the beam AB as mm. (Figure: I=300x106 mm4, E=200 GPa, P=200 kN, L=4.5 m, a=1.2 m)(d) Using the singularity function method, express the deflection y for the entire beam ABC as the equation for x (including E, I, P, a, L).(e) And use the following values to represent the deflection value yC at the right end part C as mm. (I=300x106 mm4, E=200 GPa, P=200 kN, L=4.5 m, a=1.2 m)OK EFyz0 Example The figure shows two rollurs and in equilibrium. Find the valus of the reachion foras Ra and Ry of the rollers on the beam. The beam is weightluss. laterally loaded beam which is supported by a 400N 800N 200N 10ON 800 min So 000 m Solution 200 mm 300 mm 800N EFy z0 400N 200N joON 0-3 2.7 Ra tR - 200 - 400+ 100 -800 =0 Ra Rat Ry s 1300 Ra 1300- Rb ZMa z0 -(200x 0.6) + (400 0-2) - (100* 0.7) -(R 1) + (800 * ) = 0 - 120 + 80 -70 - R + 1360 -0 RE. 1360 t80 -120-10 1250 N * Ra : 13o0 - 1250 = 50 N. HW Repeat the Salution by taking the moment a boud O O General two dimen sional_fora system Fx=0, ZFyProblem 1: (Please solve parts A and B of problem) A) A uniformly distributed load is subjected on the clamped-clamped beam and it is supported by a spring in the middle of the beam. Using Castigliano’s theorem, find the deflection in the spring. (Please use only Castigliano’s theorem to solve this part) B) Remove the spring in part A and use the Rayleigh-Ritz method to solve for the deflection at the middle of the beam. Assume that v(x) = C (1- Cos((2Pi*x)/L)) (Please use only Rayleigh-Ritz method for this part)A beam of uniform rectangular section 200 mm wide and 300 mm deep is simply supported at its ends. It carries a uniformly distributed load of 9 KN/m run over the entire span of 5 m. if the value of E for the beam material is 1 X 104 N/mm2 , find the slope at the supports and maximum deflection. Give me complete solution based on the given above. Again I need to ask the same question since you gave me a wrong answer before.> Next question You can retry this question below A triangular distributed load of max intensity w-490 N/m acts on beam AB. The beam is supported by a pin at A and member CD, which is connected by pins at C and D respectively. Determine the reaction forces at A and C. Enter your answers in Cartesian components. Assume the masses of both beam AB and member CD are negligible. cc 030 BY NC SA 2016 Eric Davishahl Variable Value 6.6 m a b C D 11.88 m 4.95 m Values for dimensions on the figure are given in the following table. Note the figure may not be to scale. The reaction at A is A = -11268.69 N. The reaction at Cis C= 11268.69 N. 20 Submit Question Jump to Answer X2-3923.92 B X2+ -8451.52 H X XThe dimensions are of the graph are d1 = 7 cm , L1 = 6 m , d2 = 4.2 cm , and L2 = 5 m with applied loads F1 = 130 kN and F2 = 60 kN . The modulus of elasticity is E = 80 GPa . Use the following steps to find the deflection at point D. Point B is halfway between points A and C. What is the reaction force at A? Let a positive reaction force be to the right.The beam shown below is supported by rollers at A and B, and by a pin at C. If EI is constant over the length of the beam, find the reaction forces at A, B, and C. 15 kip AT 6 ft B_ 6 ft 12 ft 3 kip/ft CBP4: A simply supported beam of constant El and length L is supporting a distributed load omega w over half of its length from 0 to L/2. Determine the deflection of the beam at L/2 using Catigliano's method.For the beam and loading shown in Figure 5, determine the value of (r) at the point of action of the resuitant force of the distributed load using point B as the origin. Parabola Vertex 2000 N/m 900 N/m B 6 m A Figure 5: A parabolic distributed load on a beam AB. Answer: If the loading were analysed using point A as the origin, would the value of w at the location of the resultant change? Select one: a. No b. YesL by the double integeration method. E = 200 GPa , I = 20 X10ʻmm“, and L = 3.0 m._Extra points will be added if you also model it using RISA-2D software. Send me the model file, the deflected shape in a PDF file Compute the values of slope and deflection for the beam shown below at x = with the maximum deflection values, and a screenshot (image) for the deflection value at the pointL shown on the deflected shape. 350 KN/m 70 KN/m 400 KN.m4. If a lion lies stretched out over the entire length of the branch in question 3, exerting a constant force of over the entire length of the and . The boundary conditions are branch. It is given that . Use your notes to model the fourth order differential equation suited to this application. Present you differential equation with the equation. Use direct integration and solve this equation in terms of subject of . Determine the deflection (in terms of entry. ) at . Do not use Matlab as its solu tion will not be identif You must indicate in your solution: 1. The simplified differential equation in terms of the deflection i able in the solution you will be solving 2. All the steps associated with direct integration 3. The substitution process required for determining constants of integration 4. Express the solution and determine th3. Determine the displacement and slope (i.e. 0) at the load point for the stepped beam shown in the following figure. Also determine the reaction forces and moments. Each element has E = 200 GPa. The area moment of inertia are given as I₁ = 1.25 × 105 mm4, and 2 = 4 x 104 mm. Clearly show the elemental stiffness matrices (k) for each element, assembly of k matrices to get global stiffness matrix (K) and application of boundary conditions. Then solve the reduced K matrix to get displacements and reactions 3000 N 150 mm 75 mm 125 mmSEE MORE QUESTIONS