PROBLEM 01: Considering a W24x104 section for the beam Properties of the W24 x 104 sectionshown, check whether this member satisfies the appropriate Ag = 19742 mm2AISC interaction equation. Assume the beam section to be d = 611.12 mmcompact and use A36 steel. The horizontal beam-column issubjected to a service live load P=125 kN and Q = 800 kN. bi = 323.85 mmConsider the weight of the beam. The member is laterally t = 19.05 mmbraced at its end and the bending is along it major axis. k = 1290 x 10 mm+Lateral supports are provided at the X marks. Use LRFD and ly = 108 x 10 mm4AISC specificationstw = 12.70 mmSx = 4228 x 103 mm3Sy = 667 x 10° mmnominal weight = 155 kg/mZx = 4736 x 103 mm3Zy = 1023 x 103 mm3IPQ2m4mEDIFICA

y = d/2 = 611.12/2 = 305.56 w = 155 x 9.81 = 1.52KN/m wu = 1.2x1.52 = 1.83 KN/m Pu = 1.6x125 = 200…

PROBLEM 01: Considering a W24x104 section for the beam Properties of the W24 x 104 section shown, check whether this member satisfies the appropriate AISC interaction equation. Assume the beam section to be d = 611.12 mm compact and use A36 steel. The horizontal beam-column is tw = 12.70 mm subjected to a service live load P=125 kN and Q = 800 kN. bị = 323.85 mm Consider the weight of the beam. The member is laterally = 19.05 mm braced at its end and the bending is along it major axis. k = 1290 x 10° mm Lateral supports are provided at the X marks. Use LRFD and ly = 108 x 10 mm4 AISC specifications Ag = 19742 mm2 Sx = 4228 x 103 mm Sy = 667 x 10° mm Zx = 4736 x 10° mm3 Zy = 1023 x 103 mm3 nominal weight = 155 kg/m Q 2m FICA 4m

PROBLEM 01: Considering a W24x104 section for the beam Properties of the W24 x 104 section shown, check whether this member satisfies the appropriate AISC interaction equation. Assume the beam section to be d = 611.12 mm compact and use A36 steel. The horizontal beam-column is tw = 12.70 mm subjected to a service live load P=125 kN and Q = 800 kN. bị = 323.85 mm Consider the weight of the beam. The member is laterally = 19.05 mm braced at its end and the bending is along it major axis. k = 1290 x 10° mm Lateral supports are provided at the X marks. Use LRFD and ly = 108 x 10 mm4 AISC specifications Ag = 19742 mm2 Sx = 4228 x 103 mm Sy = 667 x 10° mm Zx = 4736 x 10° mm3 Zy = 1023 x 103 mm3 nominal weight = 155 kg/m Q 2m FICA 4m

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

PROBLEM 2. The lap joint in the figure is made using a 30 mm diameter bolt. The outer plates are 5 mm thick, made of 2014- T6 aluminum and the inner plate is 10 mm thick and made of 6061-T6 aluminum. The bolt is made of S355 steel material. Calculate the load P that the lap joint can safely support, taking into account the failure of the plates by shear and tension and failure of the bolt by bearing and shear. Use a factor of safety for ultimate strength of F.S.=1.5 100 min 20 m P/2 P/2
determine the member stresses of the truss shown. indicate if the stress in the member is in tension or compression. present complete and neat solutions. p1-30kN W-25kN/m P2=51kN AH Av Im P₂ Im P₂ Im P₂ Im Av W 1.6m
Determine the design strength of a T-Beam with the following data: b+= 700 mm bw = 300 mm hy = 100 mm d = 500 mm f₂ = 21 MPa fy = 414 MPa A: 5-20 mm dia.
For the beam and loading shown, check if the maximum bending stress is less than the allowable bending stress using the ASD approach. The self-weight of the beam is denoted "waw", and the steel beam is a "W10x26". Assume the beam has an allowable stress due to bending of 21 ksi. See the next page for section properties of the steel beam. Assume the steel cross-section is being bent about its "strong axis" - i.e. the "x-axis". PL = 5.0 kip Wsw B 10 ft
NO. 1. What is the maximum bending stress in the uniformly loaded cantilever beam as shown if the depth of the beam is h = 250mm, the maximum deflection is 8max = 5mm, the span is L = 3m, and the modulus of elasticity is E = 70 GPa. Use any method. Wo L max A B 4-T
Rigid member BED is supported using steel rods AB, CD, and EF as shown below. E-200 GPa for steel. If a force P is applied at E, determine: a) The stress in each rod b) The length of each rod after applying the force LI (mm) LI (mm) P (kN) AAB (mm2) ACD (mm?) AEF (mm) 395 350 20 250 250 450 L1 L2 Note: BE ED P.
Determine the design strength of a T- Beam given the following data: bf = 700 mm bw = 300 mm hf = 100 mm d = 500 mm fc' = 21 MPa fy = 414 MPa As: 5- 20 mm dia.
A cantilever beam having a 4m span carries a uniformly distributed load throughout its length. The beam is A36 steel with yield strength Fy = 248 MPa. The beam is not restrained against lateral buckling. The beam is W 21 by 62 steel shape, whose relevant properties are shown below: r = 0.053 m d = 0.533 m bf = 0.210 m tf = 0.016 m S = 0.002077 m3 Given this condition, solve for the allowable flexural stress in the compression flange. Use Cb = 1 as should be taken conservatively
A lightly welded steel beam shown in Figure 5 is continuously supported along its length. A downward concentrated load of 4P acts at Point C, and two downward concentrated loads P act at Points A and E. The beam with full lateral restraint is bent about its major principal x-axis. Determine the followings: a. Section type based on section slenderness; b. Effective section modulus; c. The maximum design value of P. A k B fu 6 m d tw bf 6 m tf 4P d bf tw tf = - = fyf= fyw 6 m D um * 550 mm 206 mm 6 mm 10 mm 320 MPa = 340 MPa Zx=1362985 mm³ Sx 1533750 mm³ Figure 5 Steel beam under design loads. 6 m P E
SOLVE please Determine the design bending strength of ISLB 350 @ 486 N/m, considering the beam to be laterally supported. Assume factored design shear force will not exceed 0.6 times the design shear strength of the cross-section. If it is used as simply support beam of unsupported length 5 m then determine the factored distributed load the beam can carry. Use Fe410 grade steel For ISLB 350 @ 486 N/m, section properties are as follows: h = 350 mm; b= 165 mm; t₁ = 11.4 mm; t = 7.4 mm; R₁ = 16 mm; Izz = 13158.3 × 104 mm²; I = 631.9 × 10¹ mm²; Zpz = 851.11 × 10³ mm³; Zez = 751.9 x 10³ mm³
Plase answer questions from (d)
Determine the design strength of a T- Beam given the following data: b = 700 mm by = 300 mm hf = 100 mm d = 500 mm fe' = 21 MPa fy = 414 MPa As: 5- 20 mm dia.