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Structural Concrete - Hassoun

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552 Chapter 15 Design for Torsion<br />

13. A. E. McMullen and V. S. Rangan. “Pure Torsion on Rectangular Sections, a Reexamination.” ACI Journal<br />

75 (October 1978).<br />

14. H. T. Solanki. “Behavior of Reinforced <strong>Concrete</strong> Beams in Torsion.” Proceedings of the Institution of<br />

Civil Engineers75 (March 1983).<br />

15. Alan H. Mattock. “How to Design for Torsion.” In Torsion of <strong>Structural</strong> <strong>Concrete</strong>. Special Publication<br />

18. American <strong>Concrete</strong> Institute, Detroit, MI, 1968.<br />

16. T. C. Hsu and E. L. Kemp. “Background and Practical Application of Tentative Design Criteria for Torsion.”<br />

ACI Journal 66 (January 1969).<br />

17. D. Mitchell and M. P. Collins. “Detailing for Torsion.” ACI Journal 73 (September 1976).<br />

18. T. C. Hsu. Unified Theory of Reinforced <strong>Concrete</strong>. CRC Publication, Boca Raton, FL, 1993.<br />

19. American <strong>Concrete</strong> Institute (ACI). “Building Code Requirements for <strong>Structural</strong> <strong>Concrete</strong>.” ACI 318-14.<br />

ACI, Detroit, MI, 2014.<br />

20. B. J. Wilson and J. F. Quereau. “A Simple Method of Determining Stress in Curved Flexural Members.”<br />

Circular 16. University of Illinois Engineering Exp. Station, Urbana-Champaign, 1925.<br />

21. S. Timoshenko. “Bending Stresses in Curved Tubes of Rectangular Cross Sections.” Trans. ASME 45<br />

(1923).<br />

22. S. Timoshenko. Strength of Materials. Van Nostrand, New York, 1930.<br />

23. R. J. Roark and W. C. Young. Formulas for Stress and Strain, 5th ed. McGraw-Hill, New York, 1975,<br />

pp. 209–285.<br />

PROBLEMS<br />

For each problem, compute the cracking moment φT cr and the maximum factored torque φT n that can be<br />

applied without using torsional web reinforcement. Use f c ′ = 4ksiandf y = 60 ksi.<br />

15.1 A rectangular section with b = 16 in. and h = 24 in.<br />

15.2 A rectangular section with b = 12 in. and h = 20 in.<br />

15.3 A T-section with b = 48 in., b w = 12 in., t = 4 in., and h = 25 in. Assume flanges are confined with<br />

closed stirrups.<br />

15.4 A T-section with b = 60 in., b w = 16 in., t = 4 in., and h = 30 in. Assume flanges are confined with<br />

closed stirrups.<br />

15.5 An inverted L-section with b = 32 in., b w = 14 in., t = 6 in., and h = 24 in. The flange does not have<br />

closed stirrups.<br />

15.6 An inverted L-section with b = 40 in., b w = 12 in., t = 6 in., and h = 30 in. The flange contains confined<br />

closed stirrups.<br />

15.7 Determine the necessary web reinforcement for a simple beam subjected to an equilibrium factored<br />

torque T u = 220 K ⋅ in. and V u = 36 K. The beam section has b = 14 in., h = 22 in., and d = 19.5 in., and<br />

is reinforced on the tension side by four no. 9 bars. Use f c ′ = 4ksiandf y = 60 ksi.<br />

15.8 Repeat Problem 15.7 using f c ′ = 5ksi and f y = 60 ksi.<br />

15.9 The section of an edge (spandrel) beam is shown in Fig. 15.17. The critical section of the beam is<br />

subjected to an equilibrium torque T u = 300 K ⋅ in. and a shear V u = 60 K. Determine the necessary<br />

web reinforcement using f c ′ = 4ksi and f y = 60 ksi. Consider that the flange is not reinforced with<br />

closed stirrups.<br />

15.10 Repeat Problem 15.9. Considering that the flange is effective and contains closed stirrups.<br />

15.11 The T-section shown in Fig. 15.18 is subjected to a factored shear V u = 28 K and a factored equilibrium<br />

torque T u = 300 K ⋅ in. and M u = 250 K⋅ft. Design the necessary flexural and web reinforcement. Use<br />

f c ′ = 4ksiandf y = 60 ksi.<br />

15.12 Repeat Problem 15.11 if V u = 36 K, T u = 360 K ⋅ in., M u = 400 K⋅ft, and h = 24 in.<br />

15.13 Repeat Problem 15.11 using f c ′ = 3ksiandf y = 60 ksi.

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