A simply supported beam AC portrayed in Figure 3 is supported by a pin and roller at A and C, respectively. The beam carries a uniformly distributed load of 34 kN/m along with AC and a point load of 15 kN at B. The beam also has an elastic modulus of 200 GPa and it has a hollow cross-sectional area as illustrated in Figure 4. The moment of inertia (I) for the beam is 8.667 x 10⁹ mm². Determine the shear force and bending moment at A, B, and C by using Shear-Moment Equation Method. Construct the shear force and bending moment diagram using the answer obtained in (a). State all the principal values. Determine the location and maximum bending moment for the beam. Calculate the bending stress at point Q and shear stress at the neutral axis (N.A) of the cross-section. A 3 m 600 mm 15 kN * B Figure 3 400 mm 34 kN/m 5 m Q N.A

Structural Analysis
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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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A simply supported beam AC portrayed in Figure 3 is supported by a pin and roller at A and
C, respectively. The beam carries a uniformly distributed load of 34 kN/m along with AC and
a point load of 15 kN at B. The beam also has an elastic modulus of 200 GPa and it has a hollow
cross-sectional area as illustrated in Figure 4. The moment of inertia (I) for the beam is
8.667 x 10⁹ mm².
Determine the shear force and bending moment at A, B, and C by using Shear-Moment
Equation Method.
Construct the shear force and bending moment diagram using the answer obtained in (a).
State all the principal values.
Determine the location and maximum bending moment for the beam.
Calculate the bending stress at point Q and shear stress at the neutral axis (N.A) of the
cross-section.
A
3 m
600 mm
15 KN
*
B
Figure 3
400 mm
34 kN/m
5 m
Q
N.A
Transcribed Image Text:A simply supported beam AC portrayed in Figure 3 is supported by a pin and roller at A and C, respectively. The beam carries a uniformly distributed load of 34 kN/m along with AC and a point load of 15 kN at B. The beam also has an elastic modulus of 200 GPa and it has a hollow cross-sectional area as illustrated in Figure 4. The moment of inertia (I) for the beam is 8.667 x 10⁹ mm². Determine the shear force and bending moment at A, B, and C by using Shear-Moment Equation Method. Construct the shear force and bending moment diagram using the answer obtained in (a). State all the principal values. Determine the location and maximum bending moment for the beam. Calculate the bending stress at point Q and shear stress at the neutral axis (N.A) of the cross-section. A 3 m 600 mm 15 KN * B Figure 3 400 mm 34 kN/m 5 m Q N.A
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