USE AREA MOMENT METHOD. THANK YOU. SHOW COMPLETE SOLUTION.The trapezoidal loading is carried by the simply supported beam AB. The beam is a steel tube with thecross section shown. Determine the displacement of the beam at midspan and the slope angle of theelastic curve at end A. Use E = 200o GPa for steel.30 kN/m-80 mm,15 KN/mB3m- 70 mm

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Answered: USE AREA MOMENT METHOD. THANK YOU. SHOW…

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1730 in.4]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 210 kip-ft, P = 13 kips, LAB = 3.8 ft, LBC= 5.7 ft. МА V A Answer: (a) VA = (b) VB= LAB P B in. in. LBC C X
The assembly consists of two 20-mm diameter rods AB and CD, a 30-mm diameter rod EF, and a rigid bar G. The assembly is subjected to the loading shown, with point E located at the midpoint of BD. Take the modulus of elasticity of the rods as 100 GPa. i. Determine the horizontal displacement of point E (indicate direction, left or right). 11. If the applied loads causes the diameter of rod AB to become 20.0022 determine the Poisson's ratio of the material (to 2 decimal places). 350 mm 450 mm A B 40 kN E 60 kN 40 kN DG
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1570 in.“]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 160 kip-ft, P = 10 kips, LAB = 9.0 ft, LBC = 13.5 ft. MA A В C LAB LBC Answer: (a) VA = in. (b) Ув in.
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1500 in.“]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 150 kip-ft, P = 26 kips, LAB = 6.1 ft, LBC = 9.2 ft. MA A LAB LBC
Determine the deflection 8g at the free end of a cantilever beam AB with a uniform load of intensity q=4 kN/m acting over the middle of the length and a point load. The lenghth of beam is equal to L=3 m. The beam has flexural rigidity El=4286311 Nm². Note that upward deflection is positive. P=qL/6 A +4 3 9 L 3 13 B ↑
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I-1730 in.4]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 210 kip-ft, P = 13 kips, LAB = 3.8 ft, LBC = 5.7 ft. MA A Answer: (a) VA = (b) VB = LAB P B in. in. LBC C - X
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1620 in.4]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 190 kip-ft, P = 26 kips, LAB = 3.6 ft, LBC = 5.4 ft. %3D %3D P V. MA C LAB LBC Answer: (a) VA = in. (b) VB = in.
1. A stepped shaft is shown, the region AB is aluminum having G = 28 GPa, and the region BC is steel, having G= 80 GPa. The aluminum portion is of solid circular cross section 45 mm diameter, and the steel region is circular with 60 mm outside diameter and 30 mm inside diameter. A clockwise torsional load of 4000 N-m is applied at B, assume ends A and Care rigidly clamped. De termine the following: a. maximum shearing stress in the aluminum b. maximum she aring stress in the steel (
-2.4m- 8 mm 200 mq 8 mm 250 mm 8mm The steel beam has the cross-sectional area shown. The beam is loaded as shown with the intensity of the distributed loading w=70 kN/m. Determine the absolute maximum bending stress in the beam in MPa.

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