Given that the flexural design moment is 301 ft-k, assume that this moment is caused as a result of a uniformly distributed load that results from the self-weight of the beam and a live load to be calculated. The span of the cantilevered beam is 15-ft. Assume #4 stirrups are used as shear reinforcement and specify the spacing of the stirrups for the three shear reinforcement zones, as applicable. Assume fy = 60,000 psi and f,' = 4,000 psi. (20 pts.) %3D Using the deflection equation below, a deflection equation for a uniformly distributed load on a cantilever beam, calculate the initial deflection of the self- weight of the beam and the live load as calculated in part a). (20 pts.) If 20% of the live load is more or less sustained, calculate the long-term deflection of the sustained loads after five (5) years. (20 pts.) wl4 A = 8Ecle 6 No. 8 bars 18 in. 15.5 in. 30 in.

Given that the flexural design moment is 301 ft-k, assume that this moment is caused as a result of a uniformly distributed load that results from the self-weight of the beam and a live load to be calculated. The span of the cantilevered beam is 15-ft. Assume #4 stirrups are used as shear reinforcement and specify the spacing of the stirrups for the three shear reinforcement zones, as applicable. Assume fy = 60,000 psi and f,' = 4,000 psi. (20 pts.) %3D Using the deflection equation below, a deflection equation for a uniformly distributed load on a cantilever beam, calculate the initial deflection of the self- weight of the beam and the live load as calculated in part a). (20 pts.) If 20% of the live load is more or less sustained, calculate the long-term deflection of the sustained loads after five (5) years. (20 pts.) wl4 A = 8Ecle 6 No. 8 bars 18 in. 15.5 in. 30 in.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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