(c) Calculate the Shear Force and Bending Moments for each appropriate loadcombination at the Ultimate Limit State in a beam given that:Gk = 2 kN/m,Qk 1.5 kN/m,WK = 0.6 kN/m,Sk = 0.8 kN/m.(13 Marks)

The objective of the question is to calculate the shear force and bending moments for each…

Answered: (c) Calculate the Shear Force and…

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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A simple beam of length L = 5 m carries a uniform load of intensity q = 5.8 kN/m and a concentrated load 22.5 kN (see figure). P = 22.5 kN| 1.5 m q = 5.8 kN/m L= 5 m- The 1-1 and 2-2 axes are labeled on the cross section below. (a) Assuming oallow = 114 MPa, calculate the required section modulus S (in mm³). (At this point, disregard the weight of the beam.) mm3 Select the most economical wide-flange beam (W shape) from this table, and recalculate s (in mm), taking into account the weight of the beam. Select a new beam if necessary. mm3 H
Calculate the Bending Stress using the equation ?? = ?.?max /? , where M is the Bending Moment for each of your two beams. Also calculate the longitudinal shear ? = ?.? /?.? for each beam. Compare and discuss the results for 3 point load and 4 point load. Draw Bending moment diagram and shear force diagram for each test.
strength of materials... answer only Draw the shear-force and bending-moment diagrams for the simply supported beam shown. Determine the shear force 3.5 m to the right of point A if W = 9.9 kN/m, T = 14.75 kNm, m = 11.1 m, and n = 5.9 m. Round off the final answer to four decimal places.
PLEASE ANSWER IN 30 MINS, THANKYOU
A simply supported beam, having the following properties: 5.5 m length, Mcr = 30 kN-m, Ig = 7000x10^6 mm^4, Icr = 3000x10^6 mm^4, uniformly distributed dead load = 5 kN/m, uniformly distributed live load = 7 kN/m, Ec = 21,000 MPa. a) Determine the value of Ma (DL+LL).
Strength of Materials, i need solutions in 15 minutes please. Q/ The Inverted T section of a L - m simply supported beam has the properties shown in Fig. (4). Find the flange width (b) so that the allowable stresses( σ tension max = 30 Mpa) and (σ compression max. = 90 Mpa.)
If the allowable shear stress is 1.25 MPa of a simply supported beam loaded by a central concentrated load P and has a rectangular cross- section (120 mm wide by 300 mm deep and I = 270 x 10^6 mm^4), then = P 60 N O zero 60000 N O 30 N O 30000 KN O
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(c) Calculate the Shear Force and Bending Moments for each appropriate load combination at the Ultimate Limit State in a beam given that: Gk = 2 kN/m, Qk 1.5 kN/m, WK = 0.6 kN/m, Sk = 0.8 kN/m. (13 Marks)