Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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- 2arrow_forwardPlease, only answer part (b) of the questions.arrow_forwardProblem 2 A loaded cantilever beam is shown. E=29,000 ksi. The W16 section that will limit the total load deflection at the free end of the beam, B to 0.75 in. is most nearly: WD = 0.5 k/ft WL = 1.0 k/ft PD= 2 k B PL = 4 k Answer: W16 x L = 12 ft %3Darrow_forward
- A simply supported rectangular beam of span 'L' and depth 'd' carries a central load 'W'. The ratio of maximum deflection to maximum bending stress is A. L²/6 Ed C. L²/ 48 Ed B. L²/8 Ed D. L²/ 12 Edarrow_forward1) Consider the elevation view of an interior beam shown below. The beam has a t-shaped cross- section (the 5 in. thick slab is cast monolithically with the beam - meaning that the 22 in. deep beam has 17 in. hanging below the slab). The c-c length is 30 ft. Assume: M bw = 14 in. fc = 6 ksi Mu,neg. = 340 k.ft en = 28.5 ft Wu h = 22 in. fy = 60 ksi Mu,pos = 230 k.ft Sw = 12 ft - Length hstab = 5 in. No. 4 stirrups Column FL a. Select flexural reinforcement for the beam at midspan assuming it is singly reinforced. T- beams under positive bending are usually singly reinforced because the depth of the neutral axis in the flange is often smaller than the depth of any bars that might be present. Iterate until the design strength, Mn, exceeds M₁ by less than approximately 20%. Provide a drawing of the section design that clearly shows the location of the longitudinal reinforcement. Show the section complies with relevant ACI Building Code requirements (As,min, bar spacing limits, Et, min). b.…arrow_forward
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