Q2: For the cantilever beam with uniformly distributed load shown in Figure 2. Use the data (bf,hf ̟bw,hw) for the I section from Table 2, determine the following: The maximum shear force in the beam in (kN) The maximum bending moment in the beam in (kN.m) The area of the section in (mm²) The moment of inertia about the centroidal x axis The maximum shear stress at section 1 in (MPa) The maximum shear stress at section 2 (within the flange) in (MPa) The maximum shear stress at section 2 (within the web) in (MPa) The maximum shear stress at section 3 (at the neutral axis) in (MPa) The average shear stress on the section (MPa) 16kN/m sm bf=82 hf=20 2 3 hw=30 hf=20 bw=20
Q2: For the cantilever beam with uniformly distributed load shown in Figure 2. Use the data (bf,hf ̟bw,hw) for the I section from Table 2, determine the following: The maximum shear force in the beam in (kN) The maximum bending moment in the beam in (kN.m) The area of the section in (mm²) The moment of inertia about the centroidal x axis The maximum shear stress at section 1 in (MPa) The maximum shear stress at section 2 (within the flange) in (MPa) The maximum shear stress at section 2 (within the web) in (MPa) The maximum shear stress at section 3 (at the neutral axis) in (MPa) The average shear stress on the section (MPa) 16kN/m sm bf=82 hf=20 2 3 hw=30 hf=20 bw=20
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Transcribed Image Text:Q2: For the cantilever beam with uniformly distributed load shown in Figure 2. Use the data
(bf hf,bw, hw) for the I section from Table 2, determine the following:
The maximum shear force in the beam in (kN)
The maximum bending moment in the beam in (kN.m)
The area of the section in (mm?)
The moment of inertia about the centroidal x axis
The maximum shear stress at section 1 in (MPa)
The maximum shear stress at section 2 (within the flange) in (MPa)
The maximum shear stress at section 2 (within the web) in (MPa)
The maximum shear stress at section 3 (at the neutral axis) in (MPa)
The average shear stress on the section (MPa)
16KN/m
sm
bf=82
hf=20 I
2 3
hw=30
hf=20 1
bw=20
H.
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