Q For the beam shown in the figure do the following:- 1. Draw the shear force and bending moment diagrams. 2. Determine the value of the maximum bending moment and its location in the beam. 8 kN/m 4 m 2 m
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Q: The cross-sectional dimensions of the beam shown in the figure are a = 4.6 in., b = 5.5 in., d = 4.4…
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Q: 2) Draw shear force and bending moment diagrams of the beam and find the maximum values of the shear…
A: Shear force calculations: ∑V=0 RA+5×6+20=0RA=-30-20RA=-50kNRA=50kN upwards Bending Moment…
Q: The simply supported beam as shown in the figure supports a concentrated force of 30 kN at B and a…
A: Explanation: The stepwise procedure to solve this problem is shown in the following attached image:
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Q: The 8 m long cantilever beam shown in the figure below carries a uniformly distributed load of 10…
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Q: B: For the simply supported beam shown in the figure, write equations for the shearing force and…
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Q: For the simply supported beam shown in the figure, the location of maximum bending moment from left…
A: From the moment about the right support, From symmetry,
Q: Draw the shear force and bending moment diagrams for the beam depicted in the Figure. F F FL C E L L
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Q: QUESTION 1. Longitudinal and cross-sectional views of a beam are given in the figure below. (a) Draw…
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Q: 5.7 For the cantilever beam shown in the figure, find (a) the maximum bending stress and its…
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Q: A beam of 8 m long, loaded with uniformly distributed load on the 4 m span CE with a concentrated…
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A: For solution refer below images.
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Q: The shear diagram of a beam is shown in the figure. find a.Which of the following most nearly gives…
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Q: Ex. No. 3: Determine the values of the shear stress owing to bending at point A, B3, and C in the…
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Q: For the simply supported beam with square cross sectional area as shown in the figure below: 1.…
A: The summation of force along vertically is given as, ∑Fy=0RA+RB=3 kN+2 kN+5 kNRA+RB=10 kN Taking…
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Q: Q1: For the beam ABCD subjected to the loading shown in figure below (B internal hinge) (1) draw the…
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Q: A beam of 8 m long, loaded with uniformly distributed load on the 4 m span CE with a concentrated…
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Q: 1. Draw the shear and moment diagrams for the simply supported beam described in the Figure below 8…
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A: ANSWERING QUESTION 5.3 AS ASKED.
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Q: The beam in Figure 1; (a) Draw the Normal Force Diagram. (b) Draw the shear force diagram. (c)…
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Q: The beam whose support and loading status is given in the figure, a) Draw the shear force diagram b)…
A: Note: As per our guidelines we are supposed to answer only the first 3 sub-parts. Kindly repost…
Q: Draw the shear and moment diagrams for the beam shown in figure below. Write down the name of this…
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- The horizontal beam ABC of an oil-well pump has the cross section shown in the figure. If the vertical pumping force acting at end C is 9 kips and if the distance from the line of action ofthat force to point B is 16 ft, what is the maximum bending stress in the beam due to the pumping force?The cross section of a bimetallic strip is shown in the figure. Assuming that the moduli of elasticity for metals A and B are EA=168 GPa and EB= 90 GPa, respectively, determine the smaller of the two section moduli for the beam. (Recall that section modulus is equal to bending moment divided by maximum bending stress.) In which material does the maximum stress occur?A rectangular beam with semicircular notches, as shown in part b of the figure, has dimensions h = 120 mm and h1= 100 mm. The maximum allowable bending stress in the plastic beam is emix = 6 M Pa, and the bending moment is M = 150 N · m. Determine the minimum permissible width bminof the beam.
- A rectangular beam with semicircular notches, as shown in part b of the figure, has dimensions h = 0,88 in. and h1 = 0.80 in. The maximum allowable bending stress in the metal beam is emax = 60 ksi, and the bending moment is M = 600 lb-in. Determine the minimum permissible width bminof the beam.The beam ABC shown in the figure is simply supported at A and B and has an overhang from B to C Draw the shear-force and bending-moment diagrams for beam ABC. Note: Disregard the widths of the beam and vertical arm and use centerline dimensions when making calculations.Determine the maximum bending stress emaxdue to pure bending by a moment (M) for a beam having a cross section in the form of a circular core (see figure). The circle has diameter d and the angle ß = 60°. Hint: Use the formulas given in Appendix E, Cases 9 and 15.
- The cross section of a rectangular beam having a width b and height h is shown in part a of the figure. For reasons unknown to the beam designer, it is planned to add structural projections of width b/9 and height d/9 the top and bottom of the beam (see part b of the figure). For what values of d is the bending-moment capacity of the beam increased? For what values is it decreased?Determine the fixed-end moments (MAand MB) and fixed-end forces (R4and Rs) for a beam of length L supporting a triangular load of maximum intensity q0(see figure). Then draw the shear-force and bending-moment diagrams, labeling all critical ordinates.A beam of length L is designed to support a uniform load of intensity q (see figure). If the supports of the beam are placed at the ends, creating a simple beam, the maximum bending moment in the beam is qL2/8. However, if the supports of the beam are moved symmetrically toward the middle of the beam (as shown), the maximum bending moment is reduced. Determine the distance a between the supports so that the maximum bending moment in the beam has the smallest possible numerical value. Draw the shear-force and bending-moment diagrams for this condition. Repeat part (a) if the uniform load is replaced with a triangularly distributed load with peak intensity q0= q at mid-span (see Fig. b).
- Draw the shear-force and bending-moment diagrams for a cantilever beam AB acted upon by two different load cases. A distributed load with linear variation and maximum intensity q0(see figure part a). A distributed load with parabolic variation and maximum intensity q0(see figure part b).A beam supporting a uniform load of intensity q throughout its length rests on pistons at points A, C and B (sec figure). The cylinders are filled with oil and are connected by a tube so that the oil pressure on each piston is the same. The pistons at A and B have diameter d1and the piston at C has diameter D2. (a) Determine the ratio of d2to d1so that the largest bending moment in the beam is as small as possible. Under these optimum conditions, what is the largest bending moment Mmaxin the beam? What is the difference in elevation between point C and the end supports?The cross section of a sand wie h beam consisting of aluminum alloy faces and a foam core is shown in the figure. The width b of the beam is 8.0 in, the thickness I of the faces is 0.25 in., and the height hcof the core is 5.5 in. (total height h = 6.0 in). The moduli of elasticity are 10.5 × 106 psi for the aluminum faces and 12.000 psi for the foam core. A bending moment M = 40 kip-in. acts about the z axis. Determine the maximum stresses in the faces and the core using (a) the general theory for composite beams and (b) the approximate theory for sandwich beams.