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Structural Concrete - Hassoun

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11.14 Biaxial Bending 397<br />

5 no. 10<br />

5 no. 10<br />

Figure 11.22 Example 11.16.<br />

4. Check the chosen section by statics similar to Example 11.3.<br />

a. Determine the value of a using the general equation Aa 2 + Ba + C = 0 with e ′ = e + d −<br />

h/2 = 38.5 in., A = 0.425 f c ′ b = 27.2, B = 2A(e′ − d) =1033.6, C = A ′ s (f y − 0.85f c ′)(e′ − d +<br />

d ′ )−A s f y e ′ =−6941.2. Solve to get a = 5.82 in. and c = a/0.85 = 6.85.<br />

b. Check f s ′:<br />

( )<br />

f s ′ c − d = 87 ′ ( ) 6.85 − 2.5<br />

= 87<br />

= 55.26 ksi<br />

c<br />

6.85<br />

Let f s ′ = 57 ksi.<br />

c. Recalculate a:<br />

C = A ′ s (f ′<br />

s − 0.85f ′ c )(e′ − d + d ′ )−A s f y e ′ =−7351<br />

Solve now for a to get a = 6.13 and c = 7.21 in.<br />

d. Check f s ′:<br />

( )<br />

f s ′ c − 2.5<br />

= 87 = 56.83 ksi<br />

c<br />

Calculate<br />

C c = 0.85(4)(6.13)(16) =333.5K C s = A ′ s (f s ′ − 0.85f c ′ )=6.35(57 − 0.85 × 4)<br />

= 340.4 K T = A s f y = 6.35(60) =381 K<br />

e. Let P n = C c + C s − T = 292.9 K.<br />

5. Determine φ: ε t = [(d t − c)/c] 0.003 = 0.00511. Because ε t = 0.00511 > 0.005, φ = 0.9.<br />

6. Because φP n = 0.9(292.9) = 263.6 K > 257 K, the section is adequate.<br />

11.14 BIAXIAL BENDING<br />

The analysis and design of columns under eccentric loading was discussed earlier in this chapter,<br />

considering a uniaxial case. This means that the load P n was acting along the y-axis (Fig. 11.23),<br />

causing a combination of axial load P n and a moment about the x-axis equal to M nx = P n e y or

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