(a)
Wu=1.2(D.L)+1.6(L.L)
WU=1.2(.75)+1.6(1)
Wu=2.5 kip/ft
M=WuL2/8
M=2.5x(30)2/8
M=281.25 ft-kips
(b)
Shear of the beam=wL/2=2.5x30/2=37.5 kips
Deflection limit=L/360=30X12/360=1 in
Select a W section based on Zx value:
Zx>M/(Fy)
Zx>281.25x12/(0.9x50)
Zx>75 in3
The Section should have design strength more than 281 kip-ft
The section should have shear 37.5 kips
The section should have live load deflection less than 1 in
All these are satisfied by W18X55 only
(c)
Consider for the moment gradient
Cb=1.30 for UDL with simply supported beam and braced at middle
M/Cb=281.25/1.30=216.3 ft-kips
The Zx value for the beam should be greater than 75 in3 from the previous step,and the LRFD moment value should be greater than 281 ft-kips
there are two possibilities
W14X48 and W12X53,for design purposes prefer the steel which is having lesser weight
Prefer W14X48
(d)
Adequacy of W14X48
Mu=281 ft-kips
M=FyZx=50x78.4=3920 in-kips
Design strength=0.9*3920/12=294 ft-kips
So Mn>Mu (This is safe)
Shear:
Shear force=WL/2=2.5x30/2=37.5 kips
From the Zx tables, Vn=141 kips
Vn>Vu
So it is safe in shear
Deflection:
Maximum permissible deflection=L/360=30*12/360=1 in
Deflection =5wL4/384EI=5x1/12x(30x12)4/384x29000x484=1.30 in
W14X48 is not adequate in live load deflection, adopt for sections having higher moment of inertia
Show all steps Problem 1: Select a W-shape beam for the following load scenario. Assume there...
Please show all steps and cite all AISC formulas. Thanks 5) Compression combined with bending - design AW-section beam-column member is to be used in a braced frame, and must support factored LRFD loads of Pu 600k and moments Mux = 330 k*ft (these loads were derived through use of a rigorous 2nd-order analysis and include notional loads). The member is 18ft long and totally unbraced with respect to both flexural buckling (for compression) and lateral-torsional buckling (for flexure). Choose...
Select the lightest designated W14x section (A992) for the load condition given below assuming the member is fully braced against lateral torsional buckling and no holes: Pu = 400 kips (tension) Mux = 300 kip-ft Muy = 0 kip-ft Make use of AISC-15 Table 6-2 but verify selection using more detailed calculations, tables and beam charts.
Problem l The beam shown below is laterally braced at D,F and F. The uniform load shown does not include the weight of the beam. Determine whether a W24x 104 ASTM A992 is adequate for bending and shear. P,-12k PL -36k 3k/ft 10 20 30 FIGURE P5.5-15 a) Determine the controlling load combination and calculate Pu (for the concentrated force) and wu (for wo plus beam's selfweight, which is a uniformly distributed load) b) Analyze the beam loaded with the...
Please refer AISC 15th edition 2. Select the lightest W shape to carry a uniformly distributed dead load of 0.5 kips/ft and a live load of 1.0 kips/ft on a simply supported span of 42 ft. Adequate lateral support is provided. The live load deflection is limited to 360, Use A572 Grade 50 steel and LRFD. (credit weight 30)
Problem 3: Design of Steel Beam for Bending with Varying Unbraced Lengths Select the lightest A992 steel W-shape for the beam shown below using LRFD. Only consider design (neglect shear a bracing situations: a. Continuous lateral support of the compression flange b. Lateral support at beam ends and at the point of the concentrated load c. Lateral support only at beam ends PD = 10k PL-20k WD-3.33 k/ft w, = 6.67 k/ft 10' 20' 30'
Problem 2. Design and select an ASTM A992 (Fy" 50 ksi) W-shape column to carry an axial dead load of 140 kips and live lond of 420 kips. The column is 30 feet long, and is pinned top and bottom in both axes. In addition, the column is laterally braced about the y-y axis (local weak/minor axis of the section) and torsionally braced at the midpoint. Limit the column size to a nominal 14 in. shape, that is W14 shape...
Problem# 1: Determine the location of the centroid. Determine the moment of inertia about horizontal and vertical cen 2" 2 6 Problem#1 : Select a solid, rectangular, Eastern hemlock beam for a 20 ft simple span carrying a superimposed uniform load of 325 lb/ft (15 points) Problem#2: Select the wide flange steel girder for a simple span of 36 ft subjected to a concentrated load of 215 kips at the midspan. Use A36 steel and assume that beam is supported...
The single-story unbraced frame shown below is subjected to dead load, roof live load, and wind load Figure 1 shows the results of a first-order analysis relative to the columns of the frame. The axial load and end moment (also equal to the maximum moment in the column) are given separately for the different load cases (i.e., dead load, roof live load, and lateral wind load). All vertical loads are symmetrically placed and contribute only to the Mnt moments (i.e.,...
Problem 1 (100 pts) Select the lightest W24 beam section with Fy = 50 ksi using LRFD for the following span and loading. The unbraced length of the compression flange is 30 ft (Lb = 30'). Consider Cb > 1. The given dead load does not include beam weight. Verify that the selected beam has adequate shear strength. Maximum allowable deflection due to live load is L720. Maximum allowable deflection due to total load is L/360. WD = 1.2 k/ft...