1. Given the beam below, find the following: -- A a. The factored load on the beam using LRFD method. b. The factored moment demand using LRFD method. c. Assess whether the beam is safe under bending if the nominal moment is 95 kN-m, and the strength reduction factor is 0.9. Provide mathematical evidence of your assessment. DL = 1.7 KN/m; LL = 2.9 KN/m 10 m B

1. Given the beam below, find the following: -- A a. The factored load on the beam using LRFD method. b. The factored moment demand using LRFD method. c. Assess whether the beam is safe under bending if the nominal moment is 95 kN-m, and the strength reduction factor is 0.9. Provide mathematical evidence of your assessment. DL = 1.7 KN/m; LL = 2.9 KN/m 10 m B

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

Please show detailed workings for easier understanding. Thank you. (Model Ans: For AB = 50kN ; For BCD = 175kN ; For DE = 240kN)
find all ractions using congucate beam method . with deflection table
Determine the maximum bending stress (in Pa) for the beam shown belowif P = 1684 N, T = 4250 Nm, a = 0.62 m, b = 0.96 m, c = 0.92 m, w = 43 mm, and h = 70 mm. Round off the final answer to two decimal places. P T + AO А h B ka b C C ļ D
complete solution please with FBD
ASAP!!! NEED RIGHT COMPLETE SOLUTION !!!
Detailed Solution please
QUESTION: The distributed load on the T-section beam shown below and moment affects. A is the fixed joint and B is the sliding joint. This beam is made of a ductile material with a yield stress (σak) of 1000 MPa. The thickness (depth) of the beam profile is t=6 mm. A) As a mechanical engineer, check the strength of this beam (in terms of Normal and Shear Stress) ? B) In order for the existing beam to run smoothly, two 100x25 mm plates made of the same material are planned to be welded to this beam. The mechanical engineer working in the factory told the welder to weld this piece under the beam (where the B point is). But the welder, regardless of what the mechanical engineer said, welded this plate to both sides of the existing T-section beam as shown below, thinking that it wouldn't matter anyway. As a mechanical engineer : 1) After welding these plates on both sides of the beam, as the welder did, find out whether the new beam will work smoothly or not by making the necessary…
The beam is subjected to a shear of V = 13.5 kN. Set w = 125 mm. (Figure 1) Part A Determine the web's shear stress at A. Express your answer to three significant figures and include the appropriate units. HA igure 1 of 1> Value Units 200 mm Submit Request Answer 30 mm Part B 25 mm Determine the web's shear stress at B. Express your answer to three significant figures and include the appropriate units. 250 mm HẢ 30 mm Value Units
answer only d and e
The beam shown below with a length L = 16 m and a rectangular cross section that has a width of b = 50 mm and a depth d = 150 mm, has a load applied a x = 3 m away from the left hand support. What is the maximum load P that can be applied on the beam if the maximum bending stress can't exceed 14.0 MPa. Ignore any load factors or strength reduction factors.
A) Determine the shape factor and the Fully Plastic Moment (Mp) for the shaded symmetrical hollow rectangular beam section shown below. Assume the yield stress Oy =275 N/mm?. B) If two plates of width 250 mm and thickness equal to 't' mm is connected (fabricated) at top and bottom (one plate on each side) for the given section, then what is the improvement in the fully plastic moment(Mp) of the section. C) If this revised fabricated section is now rotated by 90 degrees, what is its effect on the shape factor of the section? 200 mm. -50 mt 100 mm 400 50m Note : Take the value the 't' as equal to the last two digits of your student id. If the last wo digits are zero then takes T=10mm ww 00T
Week: 3: Flexure: Behavior and Nominal Strength of Beam Sectio 3.6 The Working-Stress Design Method * Homework 1: Calculate the bending stresses for the section shown. Use M = 55 kN.m f'e= 27.6 Mpa 250 mm fy = 414 MPa 535 mm 600 mm As-1516 mm Ausinan atesser O anan ama