Thesimply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; 1= 351 x 106 mm*]. Determinethe beam deflection at point A.(a)(b) the beam deflection at point C.Assume P = 39 kN, w = 61 kN/m, LAB= 3.6 m, LBC= 3.6 m, LcD = 3.6 m, LDE = 1.8 m.Answer:VA=PVc =IBLABLBCmmmmLCDWDLDEEX

EI = 200*103 x 351*106 = 70.2*1012 Nmm2

The simply supported beam consists of a W530 x 66 structural steel wide-flange shape [E = 200 GPa; 1= 351 x 10 mm4]. Determine (a) the beam deflection at point A. (b) the beam deflection at point. C. - Assume P = 39 kN, w=61 kN/m, LAB = 3.6 m, Lec-3.6 m, LcD = 3.6 m, LDE = 1.8 m. Answer: VA = P Vc = B LAB LBC m 1 mm mm LCD W D LDE E X

The simply supported beam consists of a W530 x 66 structural steel wide-flange shape [E = 200 GPa; 1= 351 x 10 mm4]. Determine (a) the beam deflection at point A. (b) the beam deflection at point. C. - Assume P = 39 kN, w=61 kN/m, LAB = 3.6 m, Lec-3.6 m, LcD = 3.6 m, LDE = 1.8 m. Answer: VA = P Vc = B LAB LBC m 1 mm mm LCD W D LDE E X

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; I = 351 x 10^6mm^4]. Determine (a) the beam deflection at point A. (b) the beam deflection at point C. Assume P = 30 kN, W = 59 kN/m, LAB = 3.2 m, LBC = 3.2 m, LCD = 3.2 m, LDE = 1.6 m.
The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; I = 351 × 106 mm4]. Determine the beam deflection at point C. Assume MA = 280 kN·m, w = 125 kN/m, P = 150 kN, MD = 200 kN·m, LAB = 3.4 m, LBC = 1.7 m, LCD = 2.6 m.
Need asap pls. Thank you.
The simply supported beam consists of a W24 × 94 structural steel wide-flange shape [E = 29,000 ksi; I = 2,700 in.4]. For the loading shown, determine the beam deflection at point C.Assume P = 39 kips, w = 2.7 kips/ft, LAB = 13 ft, LBC = LCD = 7 ft.
Problem 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 %3D
The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; I = 351 × 106 mm4]. Determine(a) the beam deflection at point A.(b) the beam deflection at point C.Assume P = 44 kN, w = 87 kN/m, LAB = 4.0 m, LBC = 4.0 m, LCD = 4.0 m, LDE = 2.0 m.Answer:vA = mmvC = mm
In the following beam with the working section shown is subjected to the indicated loads and supported as shown, determine the magnitude of the twist BA and the deflection YC in the middle. Consider E = 70 GPa, A = 7.5 x 10-3 m2, IZ = 61.3 x 10-6 m4, IY = 23.2 x 10-6 m4 Develop by: 1) Double integration method 10 kN 2) Overlay Method 3) Moment area method 4m 4 m develop: a) Problem approach and solution sequence b) Free body diagram c) Calculation of intermediate and constant forces d) Bending moment diagram e) Application of equations and associated tables Caniatidado AM 141do earde tier ade
The simply supported beam consists of a W460 × 82 structural steel wide-flange shape [E = 200 GPa; I = 370 × 10ó mm“]. For the loading shown, determine the beam deflection vc at point C. Assume P = 51 kN, w = 18 kN/m, LaB = LBC = 2.8 m, LCD = 2.2 m.
l8
The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; /= 351 x 106 mm4]. Determine the beam deflection at point C. Assume MA = 250 kN-m, w = 105 kN/m, P = 115 kN, Mp= 180 kN-M, LAB = 4.0 m, LBc = 2.0 m, Lcp =3 m. P "| W Mp B C LAB MA Answer: Vc = mm LBC LCD X
ASAP
Determine the minimum width "b" of the beam shown if the flexural stress is not to exceed 13 MPa. Answer must be in mm. Given: a = 1 m, b = 3 m, c = 2 m, P = 6 kN, and w = 3 kN/m. P kN cm w kN/m (not scaled) 250 mm am b m b. R1 R2