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Structural Concrete - Hassoun

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Summary 439<br />

3. The value of K can be determined from the alignment chart (Fig. 12.3) or Eqs. 12.2<br />

through 12.6.<br />

Section 12.4<br />

Member stiffness is EI:<br />

E c = 33w 1.5√ f ′ c<br />

The moment of inertia, I, may be taken as I = 0.35I g for beams, 0.70I g for columns, 0.70I g<br />

for uncracked walls, 0.35I g for cracked walls, and 0.25I g for plates and flat slabs.<br />

Alternatively, the moments of inertia of compression and flexural members, I, shall be permitted<br />

to be computed as follows:<br />

1. Compression members:<br />

(<br />

I = 0.80 + 25 A )(<br />

st<br />

1 − M )<br />

u<br />

A g P u h − 0.5P u<br />

I<br />

P g ≤ 0.875I g<br />

o<br />

2. Flexural members:<br />

(<br />

I =(0.10 + 25ρ) 1.2 − 0.2 b )<br />

w<br />

I<br />

d g ≤ 0.5I g<br />

(Eq.12.2)<br />

(Eq.12.3)<br />

Section 12.5<br />

The effect of slenderness may be neglected when<br />

Kl u<br />

r<br />

⎧<br />

⎪<br />

22 (for unbraced frames) (Eq.12.8)<br />

≤ ⎨<br />

⎪<br />

34 − 12 M 1<br />

≤ 40 (for braced columns) (Eq.12.5)<br />

⎩<br />

M 2<br />

where M 1 and M 2 are the end moments and M 2 > M 1 .<br />

Section 12.6<br />

1. For nonsway frames,<br />

or the more simplified equation<br />

More simply,<br />

The Euler buckling load is<br />

EI = 0.2E cI g + E s I se<br />

1 + β dns<br />

(Eq.12.10)<br />

EI = 0.4E cI g<br />

1 + β dns<br />

(Eq.12.11)<br />

β dns =<br />

1.2D<br />

1.2D + 1.6L<br />

EI = 0.25E c I g (β dns = 0.6)<br />

P c = π2 EI<br />

(Kl u ) 2<br />

(Eq.12.4)<br />

(Eq.12.12)<br />

(Eq.12.13)

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