The compound heam is made from two sections, which are pinned together at B. Use Appendix...
2 - Select the lightest-weight wide-flange beam from Appendix B that will safely support the loading. The allowable bending stress is sallow - 22 ksi and the allowable shear stress is tallow 12 ksi. 5 kip 18 kip ft 6 ft 12 ft
D . Select the lightest-weight steel wide-flange overhanging beam from Appendix B that will safely support the loading. Assume the support at A is a pin and the support Jo now = 12 ks: at B is a roller. The allowable bending stress is allow = (see email data) Zaves IU KS and the allowable shear stress is allow --- 14 ksi. P=11 hip 8t 44 y. Selected beam section is: W X P (see email data for value of...
MECH3211- Stress Analysis Tutorial Assignment #6 Thursday, June 27, 2019 Student ID# Name: Problem 2: The Select the lightest-weight wide-flange beam from Appendix B that will safely support the loading. The allowable bending stress is aaltow 24 ksi and the allowable shear stress is Tallow 14 ksi. 6.75 kip/ft 12 kip 1.5 m 2 m m MECH3211- Stress Analysis Tutorial Assignment #6 Thursday, June 27, 2019 Student ID# Name: Problem 2: The Select the lightest-weight wide-flange beam from Appendix B...
***NOTE*** you *MUST draw complete FBD, and complete Shear-Force and Bending-Moment diagrams Select the lightest-weight steel wide-flange (W) overhanging beam from Appendix B that will safely support the loading. Assume the support at A is a pin and the support at B is a roller. The allowable bending stress is allow (see email data) and the allowable shear stress is "Zaitow -- 14 ksi. 8 ft + Non 4ft af Selected beam section is: W X P (kip) = 3...
A Review The allowable bending stress is allow = 24 ksi and the allowable shear stress is Tollow = 14 ksi 8 kip/It 6 ft Part A Select the lightest-weight wide-lange beam with the shortest depth from Appendix B that will safely support the loading shown Part A Select the lightest-weight wide-flange beam with the shortest depth from Appendix B that will safely support the loading shown. W12 X 16 W12 X 22 W12 X 14 W12 X 26 Previous...
The allowable bending stress is σ1ow-22 ksi and the allowable shear stress is Tallow 12 ksi. (Figure 1) Part A Select the lightest steel wide-flange beam from Appendix B that will safely support the loading shown. If there are several choicas of equal weight, choose the one with the shortest height. w14 × 26 W8 x 31 W10 × 39 w12 × 22 W12 × 26 W14 x 22 W10 × 30 W8 × 40 Submit Request Answer Figure 1...
Select a suitable wide flange section to support the beam loads shown in the figure below. Use ASTM A992 steel and allowable stresses of 0.66 Sy for bending and 0.40 Sy for shear. Be sure to generate a list of candidate beams from which, you will choose the lightest. Determine the factor of safety in bending for the beam you select. Find the deflection at the end of the overhang using the beam you selected. What is the total weight...
then considered to complete the spec"Katin. Part C Maximum Distributed Load The bending design consideration requires the calculation of the beam's section modulus. This is a property based solely on the geometry of the beam, specifically the moment of inertia and the centroid Determine the maximum uniform distributed load w that can be applied to the W12 x 14 beam shown below if the maximum allowable bending stress is Ơallow-10 ksi and the maximum allowable shear is Tallow-2.1 ksi. The...
For the loading shown, choose the lightest wide-flanged section from Appendix B that will support the loads shown with out failing. Pa = 4 Kip, P2 = 10 Kip, P3=6 Kip. Jy = 33 ksi; Ty = 18 ksi. Use a factor of safety against yield of 1.5 for both normal and shear stress. Design criteria: 1st choose lowest weight, then lowest height. The support reactions at A and B are given as shown. P. Pe P3 s' judi 4...
Learning Goal: To calculate the shear stress at the web/flange joint in a beam and use that stress to calculate the required nail spacing to make a built- up beam. A built up beam can be constructed by fastening flat plates together. When an l-beam is subjected to a shear load, internal shear stress is developed at every cross section, with longitudinal shear stress balancing transverse shear stress. If the beam is built up using plates, the fasteners used must...