- For Problems 1 Through 6 Refer To The Simply Supported Beam And Information Given Below W 547 0 10 1 20 W10x68 A36 Stee 1 (52.04 KiB) Viewed 31 times
pin and roller.
Draw clear, well-labeled shear and moment diagrams for the beam
shown.
What are the maximum bending and shear stresses in the beam?
What is the deflection of the beam 7.5’ from the roller under
the given loading?
Is the given beam sufficient? Why or why not? Assume the
deflection calculated in problem 4 is max deflection.
For Problems 1 through 6 refer to the simply supported beam and information given below: w=547 0-10 1-20 W10x68 A36 Steel Beam: FB = 22ksi Fv = 14.5 ksi WIDE FLANGE SHAPES E = 29,000 ksi Aals Y-Y Theoretical Dimensions and Properties for Designing Flange Weight Area Depth Web Sectioner of of ThichThick- Nenhet Section Section with $. A 4 in - - 5. in. n. 1. in WIB 112 2.3 11.38 10415 1.250 0.755 716 100 25.4 11.10 10.346 1.120 0.680 $23 88 25.9 10.04 10.265 0.990 0.505 534 77 22.6 10.60 10.190 0.870 0.530 455 68 20.0 10.40 10.130 0.770 0.470 394 60|17.6 10.22 10.080 0.610 1420 341 54 15.8 10.09 10.030 0.615 0.370 303 49 144 9.98 10.000 0.560 0.340 272 126 4.86 112 4.50 S.S 454 85.3 4.49 75.7 4 44 66.7 4.39 600 4.37 54.6 4.35 235 207 179 154 134 116 103 93.4 45.3 2.88 2.81 40.0 2.65 285 34.8 2.83 2.83 30.1 2.60 2.80 26.4 2.59 2.79 23.0 2.57 2.77 20.5 2.56 2.75 18.7 2.54 2.74 1. SIMPLE BEAM - UNIFORM LOAD PARTIALLY DISTRIBUTED AT ONE END REV-V (21-3) 21 R-V TR V (whon x < 4) R-WX Мин е и 2w Shear V, M, (when x < a). RX- 2 M, (when x>a) (-) WX A, (when xc a) C (21-af-2ar? (21-a)= 12") Moment