9.14 Uniformly distributed loads are applied to beam AE as shown. (a) Selecting the x axis...
A uniformly distributed load and two concentrated loads are applied to a beam as shown. Find the maximum bending moment for the beam P-10 kN P2 - 10 KN 4-2 kN/m (A) 0.0 Nm (B) 2 EN (C) 50 kNm (D) 75 kNm As shown in the following illustration, a wire connects the middle of the two links. What is most nearly the tension in the wire? 600 N/m wire 60 cm 75 cm (A) 200 N (B) 270 N...
x Incorrect Two beams support a uniformly distributed load of w = 28 kN/m, as shown. Beam (1) is supported by a fixed support at A and by a simply supported beam (2) at D. In the unloaded condition, beam (1) touches, but exerts no force on, beam (2). Beam (1) has a depth of 300 mm, a moment of inertia of 11 = 125 x 106 mm, a length of L = 3.4 m, and an elastic modulus of...
Do not round intermediate calculations. Give your final answer(s) to three significant figures. Knowing that beam A B is an S200 x 34 rolled shape and that P = 40 kN, L = 4 m, and E-200 GPa, determine the slope at A x 10rad
Question2 A steel beam is designed to carry 2 umiform distributed loads which is shown in Figure e. Apply singularity function method and refer to the properties of the rolled-steed -W shape provided in the formula sheet, choose the most economical Wshape for the beam if the maximum allowable deflection at E is 5mm. Use E 200GPa. 119 marks! 115 kN/m 75 kN/m W - Shape Figure 02
Question2 A steel beam is designed to carry 2 umiform distributed loads...
A cantilever beam supports the loads shown. The cross-sectional dimensions of the shape are also shown. Assume mm, by - 85 mm, 5 mm, 9 mm. Determine - 0.5 m, P. - 4.0 kN, Pg - 7.5 kN, Pe-2.0 kN, -85 (a) the maximum vertical shear stress. (b) the maximum compression bending stress. (c) the maximum tension bending stress. See the coordinate system for the beam in the problem figure with the origin of the x axis at the feed...
Chapter 8, Supplemental Question 067 (Go Tutorial) The simply supported beam shown carries a uniformly distributed load of w 28 kN/m on overhang BC. The beam is constructed of a Southern pine [E 12 GPa] timber that is reinforced on its upper surface by a steel [E-200 GPa] plate as shown. The beam spans are LAB-4.5 m and Lec-1.25 m. The wood beam has dimensions of bw-230 mm and dw-310 mm. The steel plate dimensions are bs - 245 mm...
The rectangular plate shown in the figure below has the given loads uniformly distributed over the edges. The plate is 50 mm thick, AB is 500 mm and BC is 400 mm (a) (b) (c) (d) (e) Determine the shear forces which must operate on the edges BC and DA to maintain the equilibrium of the plate Relative to the x,y reference axes, determine the state of stress at any point P in the interior of the plate For the...
Figure 1 shows a beam is supported by a pin at A and a roller at
C. The beam is subjected to point
loads 30 kN and 60 kN and a uniformly distributed load of 24 kN/m.
Modulus of elasticity, E and
moment of inertia, I for all members are 205 kN/mm2 and 195 x 106
mm4, respectively. By using
Virtual Work method,
(a) determine the slope at B. (1.801 mrad)
(b) determine the deflection at B and D. (2.4...
The beam is loaded as shown in the diagram below. The beam is uniformly loaded at 3 kN/m for the length of 4 m from B. The beam also has two point loads, 4 KN at 2 m from A and 3 KN at 3 m from B. 2 KN 3 KN 3KN/m A 2 m 2 m 11 m 3 m Fig. Q2 Draw a shear force and bending moment diagram. Also determine the location of maximum bending moment...
8.30. A simply supported beam with overhanging ends is loaded by
the uniformly distributed loads shown in Fig. 8-25. Determine the
deflection of the midpoint of the beam with respect to origin at
the level of the supports.
8.31. For the beam described in Problem 8.30, determine the
deflection of one end of the beam with respect to origin at the
level of the supports. Use singularity functions.
espect to origin at the level of the supporlS to 2a Fig....