The beam is simply supported. Problem 3. (30 points) A wooden beam is composed of a...
A prismatic beam with span L = 3 ft is simply supported at points A and B. The beam is supporting a uniform load with q = 160 lb/in . The cross-section of the beam is a solid rectangle with width b = 1 in and height h = 4 in . Determine: a. The normal stress (σ C ) and shear stress (τ C ) at point C located 8 inches left of support B and 1 in. below...
Problem 3: A simply supported wooden beam, 12' long, is acted on by P= 10 kip at the mid-span and a uniformly distributed load w = 1.5 kip/feet over the entire length. The nominal size of beam cross-section is 8 x 12, however, actual cross-section is 7.5 x 11.5. Calculate the maximum tensile & compressive bending stresses at the top and bottom fibers of the section. ANS: Maximum tensile & compressive stresses (o) are = . -
A simply supported beam as shown in the figure. The beam section is W18x211. The beam must support its own weight and must carry the following loading: Super-imposed distributed dead load = 0.25 kip/ft Distributed live load = 1 kip/ft Concentrated dead load = 12 kip The beam span L = 26 ft and the distance of the concentrated load from the right support a=6 ft. Consider analy- sis of beam subjected to load combination 1.2 dead + 1.6 live....
For the beam shown below, determine the flexural stresses, shear stresses, principal stresses, and the angle to the principle stress plane at the locations shown. Can you solve Location one and 4 first< then as many other as you can please? Locations 1 and 2 are at the top of the beam, while locations 5 and 6 are at the bottom. Location 3 is at the beam mid-height, while location 4 is midway between locations 3 and 5. Assume that...
2. A 30 ft long simply supported beam supports a uniformly distributed load of 2 kips/ft over the entire span. The beam and cross section are shown below. Draw the shear and moment diagrams, find the neutral axis location, moment of inertia of the composite section, the maximum bending stress on the cross section. (40 points) 10" 2 k/ft 1-3" 30'-0"
Steel Design 3. Given a. W27X84 A992 Steel beam is simply supported over a 25' FT beam length. b. The compression flange of the beam is fully braced along the beam length. c. A uniformly distributed service dead load of 2.5 KLF. d. A uniformly distributed service live load of 3.5 KLF. e. A live load deflection limit of L/360. A dead live load deflection limit of L/240. f. Neglect the self-weight of the beam in all calculations. Determine: The...
pls show work OUte 2 (25 points) A beam ABC with an overhang from B to C supports a uniform load of 220 lb/ft throughout its length. The beam is a channel section with dimensions as shown in the figure. 220 lb/ft The moment of inertia about the z axis (the neutral axis) equals 8.13 in4 A D 6 ft (A) Find the internal shear and bending moment at D. -6 ft -12 ft 990 lb 2970 lb (B) Determine...
Question 1 (6.7 points) AW12 x 50 steel beam is used as a simply supported beam on span of 24 feet. The beam supports a uniformly distributed load of 1000 lb/ft. Calculate the maximum bending stress. a) 9,560 psi Ob) 11,280 psi Oc) 13,460 psi d) none of the above Question 2 (6.7 points) Determine the number of 2 x 12's that need to be nailed together to build a beam that would support a uniform load of 500 lb/ft...
16.6a) A simply supported beam is to span 15 ft. It will support a uniformly distributed load of 2 kips/ft over the full span and a concentrated load of 60 kips at mid-span. What is the required plastic section modulus Zx? (Include self-weight) 16.6b) A simply supported beam is to span 15 ft. It will support a uniformly distributed load of 2 kips/ft over the full span and a concentrated load of 60 kips at mid-span. Deflection is not to...
Below is a diagram of a beam that is simply supported and subjected to a point load over a 9.8 in. plate. The member has 6.14 sq.-in. of flexural tension steel. You can use d = 25.7 in., bw = bv = 3.54 in., f’c = 12.2 ksi, fy = 87 ksi, Av = 0.157 sq.-in. at a spacing s = 6.50 in., finally, the maximum course aggregate used in the beams was 0.50 in. There is no axial load...