Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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- The simply supported beam consists of a W21 × 44 structural steel wide-flange shape [E = 29,000 ksi; I = 843 in.4]. Assume that the support at D can provide resistance either up or down. For a loading of w = 7.8 kips/ft, determine:(a) the beam deflection vA at point A.(b) the beam deflection vC at point C.Assume LAB = 10 ft, LBC = 8 ft, LCD = 8 ft, LDE = 7 ft.arrow_forwardUse "force method" and the table at the back of the exam to determine the reactions (all) of the statically indeterminate 2-span beam shown below. Assume EI is constant for all members. "Must use VB as the redundant reaction force". Mo = 160 ft.-k w = 1.5 k/ft. A B. НА VB Vc 20 ft. 20ft.arrow_forward6.55 Determine the axial forces in members HJ and GI. 1m 2 m 2 m 2m 2m H -6 m- 2m 2m 2m 2m 2m M 0 Q F D K I G E C B L N P R 1kN 2KN 1kNarrow_forward
- A M F B G E D a 5 m5 m 10 m 30 m 5 m The beam AF is supported by a hinge at point A and a roller at point D. A couple moment is applied at point C. Determine the internal normal force, shear force and bending moment at point G if a = 7 m, w = 19 kN/m, P = 30 kN, and M = 120 kN-m. The normal force at point G in kN is (round to the nearest integer): kN The shear force at point G in kN is (round to the nearest integer): kN The bending moment at point G in kN-m is (round to the nearest integer): kN-m P.arrow_forwardDetermine the reactions for the beam shown if the vertical deflection at support B is zero. 3.0 kip/ft O B 16' 8' SIMPLE BEAM: CONCENTRATED LOAD AT ANY POINT SIMPLE BEAM: UNIFORMLY DISTRIBUTED LOAD Pb R = V, (max when a b) R V, . Pab w V M max (at point of load). M max (at center) Pbx Shear M, (when x b) = Pab(a + 2bN3a(a + 2b) M max Amax (at center), 27EI Pah2 384EI M max Moment A, (at point of load) 3EII WX (3 – 21r2 + x³) Pbx (2 - b2 - x) 4, 24EI 4, (when xarrow_forward41. The wide-flange I beam as shown is 20 ft. Iong Itis fixed at one end and free at the other. A twisting moment of 30,000 Ib-in. is applied at the free end. If E= 30×10° psi and G = 12×1oʻ psi, compute the maximum normal and shearing stresses due to bending and the maximum shearing stress due to twist. What is the angle of twist of the beam at the free end? 10.5" 1.368" 0.845" 10" prob 41arrow_forwardarrow_back_iosarrow_forward_ios
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