The figure shows a cantilever consisting of steel angles size 100 x 100 x 12 mm mounted back to back. Using superposition, find the deflection at B and the maximum stress in the beam. 3 m - 2.5 kN 2 m I kN/m B A

The figure shows a cantilever consisting of steel angles size 100 x 100 x 12 mm mounted back to back. Using superposition, find the deflection at B and the maximum stress in the beam. 3 m - 2.5 kN 2 m I kN/m B A

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

Or A L-section beam having the dimensions, as shown in given figure is subjected to a bending moment of 1600 Nm about the y-axis. This causes tension at the top surface. Find the location of neutral axis, and maximum tensile and compressive stresses. 12 100 75 ZAH Homer N 12
I am struggling with this question
The cross-sectional dimensions of the beam shown in the figure are r = 113 mm and r;= 87 mm. Given M₂ = 16 kN-m, a = 37º, and ß = 53º, what are the bending stresses at points Hand K? H To a Part 1 Incorrect. Find the moment of inertia for a solid circular cross-section of radius 113 mm, then subtract the moment of inertia for a solid circular cross-section of radius 87 mm. Find the area moment of inertia for the cross-section about the z axis. Į₂ = mmª 7
F=20 kN single load, M=21 kN.m moment and w=20 kN/m distributed load act on the beam whose loading condition is given in the figure. The length L is given as L=6 m. The cross-sectional characteristics of the beam are body height yg= 170 mm, body thickness xg=10 mm, flange width x+=120 mm, flange height yf=10 mm. The Enocta on the beam section is located just below the flange-body junction. According to this;a) Find the support response in the y direction at point A. (Write your result in kN)b) Find the support response in the y direction at point D. (Write your result in kN).c) Find the shear force at point B. (Write your result in kN)d) Find the bending moment at point B. (Write your result in kN).e) Find the normal stress due to the bending moment at point E in the section taken from the B line of the beam. (Write your result in MPa).f) Find the shear stress due to the shear force at point E in the section taken from the B line of the beam. (Write your result in MPa).
Question 1-2) F=22 kN single load, M=23 kN.m moment and w=17 kN/m distributed load are acting on the beam whose loading condition is given in the figure . The length L is also given as L=3 m . The cross-sectional properties of the beam are; body height y g =223 mm , body thickness x g =11 mm , flange width x f = 170 mm , flange height y f =18 mm . Point E on the section is located just below the flange-body junction. It is desired to determine the stress state in the section taken from the C level of the beam. According to this; Question 1-F) For a section taken from the C point of the beam; Find the shear stress at point E on the beam section due to the shear force . ( Write your result in MPa .) Question 1-H) For a section taken from the C point of the beam; Find the normal stress that occurs at point E on the beam section due to the normal force . ( Write your result in MPa .)
solve the question given in the image.
The dimensions of a rectangular beam are limited to b = 300 mm and effective depth, d = 700 mm. Using f’c = 28 MPa, long bar fy = 415 MPa, calculate the required amount of tensile reinforcement so that a tensile strain of 0.005 is attained under a sustained ultimate bending moment of 1,200 kN.m. Compression bars centroid is 70 mm from beam edge. 4,387 3,839 6,180 5.353
As a result of the loading condition given in the I-section fixed beam shown in the figure; a)Find the maximum normal stress and the maximum shear stress b)Compare these values with the maximum stresses at point B. (Units are in mm)
Q1 A steel beam of I cross-section is simply supported on a span of 4m. Find the safe uniformly distributed load the beam can carry if the tensile stress is not to exceed (60) N/mm2. Also find the maximum compressive stress.
The built-up beam is subjected to a moment of M = 80 kNm. Variable d₁ d₂ d3 da Values for the figure are given in the following table. Note the figure may not be to scale. d5 d3 de d₁ Value 128 mm 22 mm 276 mm 11 mm 138 mm d4 12 mm M₁ de d5 a. Determine the distance from the Neutral Axis to the top of the beam, N.A. b. Determine the mass moment of inertia of the beam, I. Determine the max compressive stress acting on the beam, compression c. d. Determine the max tensile stress acting on the beam, tension.
Parvinbhai
y M B H B W Figure-2 A wide flange beam is subjected to a moment as shown in Figure-2. If M=10 kN.m, H=212 mm, W=170 mm, d=11 mm, t=18 mm and 0=64°; Btermine the momentOt lhadat about the axis- etermine the mement of inertia (mmabeut the avie y Betermine the normat stress (MPa due to bendng atpontA itic commressIive stress use Determine the orientation angle, B (degree), of the neutral axis relative to the +z axis.