3. (35p) Consider a cantilever beam of length I. and circular section of radius R. The...
A cantilever beam of a channel section is loaded at its half-length, as shown in Figure Q2. The Young's modulus of the material is 200 GPa. Determine the deflection at the free end. [12.5 marks] 25 mm 25 mm 5 kN a -a 少a 6 mm 200 mm Figure Q2 A cantilever beam of a channel section is loaded at its half-length, as shown in Figure Q2. The Young's modulus of the material is 200 GPa. Determine the deflection at...
8. The cantilever beam in Figure Q8 subjects to concentrated loading. The cross section geometry gives the second moment of area / 100 x 10 m. The longitudinal geometry of the beam: a 2 m, b 1 m. The material of the beam: Young's modulus E 200 GPa. The loading: concentrated force P 10 KN. (a) Determine the reactions to the beam at the fixed end. (b) Determine the rotation angle at point x-a (c) (Determine the deflection at the...
3. A cantilever beam of length L is embedded at its right end, and a horizontal compressive force of P pounds is applied at the free left end of the beam. When the origin is taken as its free end, the deflection of the beam can be shown to satisfy the differential equation Ely" = -Py – w(x)} Find the deflection of the cantilever beam if w(x) = Wox, 0 < x < L, and y(0) = 0, y'(L) =...
For the cantilever beam shown in figure below, we have derived the deflection curve during the lecture as: r(z)-하-둬뿌 부] 48 Consider the magnitude of the distributed load q 1 N/m, length of the beam L 1 m, Young's modulus E-200 GPa and the 2nd moment of area about the bending axis is 1 = 250 cm". What is the reaction bending moment at the left end in N.m? Ya 2
Problem 4. At one end of an elastic beam (length 2L, annular cross section with outer radius R, inner radius r, and planar moment of inertia z(R4- that is supported by a truss structure (cross-sectional area A), a vertical load P is applied, which results in a vertical deflection at that point that can be determined by 5PL 2PL3 EA 3EIz Two experiments with the same data but different inner radii r were conducted, and the deflections w were measured....
60 in 150 lbf 5 lbf/in 3. The cantilever shown in the figure consists of two structural-steel channels with a weight of 0.833 lbf/in. Both distributed load of 5 lbf/in and a point load of 150 lbf are applied to the beam as shown above. Using Castigliano's theorem find the deflection at A and compare to the deflection calculated using the superposition method. Include weight of the channels. (l3.70 in4) R A simply supported beam has a concentrated moment MA...
Consider a cantilever beam under a concentrated force and moment as shown below. The deflections ofthe beam under the force F (y) and moment M (y) are given by: 2. y' Mo L-x) , and y2 Me , where EI is the beam's flexural rigidity. The slope of the beam, 0, is the derivative of the deflection. Write a program that asks the user to input beam's length L, flexural rigidity EI (you may consider this as a single parameter,...
Q13. Consider a cantilever beam of 10m length fixed at right end. It carries 5 stones of length 2 m each placed on the beam. The load of each stone is 5 kN/m. A rod of 10 kN load is placed on the beam at 2 m from fixed end and another rod of load 12kN at midpoint of the beam. All the loads are acting downwards. Draw the beam with the loads and fixed condition. Mark the fixed end...
solve in detail Problem Statement Consider a simply supported beam with length L=1m, width w=25mm and height h. The beam has a mass m=10kg hanging from it as shown in Figure 1. The mass is located at the midpoint of the beam. Figure 1 Schematic of a simply supported beam with mass m attached to it at the midpoint. The deflection of the beam at the midpoint is given by the equation below: dmg/? 48E1 where g=9.81 m/s? is the...
DE = 29 Question 4: Indeterminate Beam Design and Deflection A 2014-T6 aluminium cantilever beam is rigidly fixed to a wall and supported at the free end with a roller support, shown below. The beam is loaded with a distributed load, W, of 10kN/m and a point load, P of 55kN. Both the distributed load and the point load act in the direction shown in the image below. Note, the parameter DE is related to your student number as described...