Civil Engineering Reference
In-Depth Information
The moment coefficients of Table 4-3 (flat plate with spandrel beams) are valid for
β t
2.5, the coefficients of
α f1 ˜ 2 / ˜ 1
Table 4-6 (two-way beam-supported slabs), are applicable when
α f1 are
stiffness parameters defined below). Many practical beam sizes will provide beam-to-slab stiffness ratios such
that
1.0 and
β t
2.5 (
β t , and
α f1 ˜ 2 / ˜ 1 and β t would be greater than these limits, allowing moment coefficients to be taken directly from
the tables. However, if beams are present, the two stiffness parameters
α f1 and
β t will need to be evaluated.
For two-way slabs, the stiffness parameter
α f1 is simply the ratio of the moments of inertia of the effective beam
and slab sections in the direction of analysis,
α f1 = I b /I s , as illustrated in Fig. 4-6. Figures 4-7 and 4-8 can be
used to determine
α f .
Relative stiffness provided by a spandrel beam is reflected by the parameter
β t = C/2I s , where I s is the moment
of inertia of the effective slab spanning in the direction of ˜ 1 and having a width equal to ˜ 2 , i.e., I s = ˜ 2 h 3 /12.
The constant C pertains to the torsional stiffness of the effective spandrel beam cross section. It is found
by dividing the beam section into its component rectangles, each having smaller dimension x and larger
dimension y, and summing the contribution of all the parts by means of the equation.
0.63 x
y
x 3 y
3
C
=
1
The subdivision can be done in such a way as to maximize C. Figure 4-9 can be used to determine the torsional
constant C.
L
L
˜ 2
Slab, I s
Beam,
I b
b
b + 2 (a - h)
b + 8h
C L
˜ 2 /2 + c 1 /2
b + (a - h)
b + 4h
Slab, I s
Beam , I b
b
c 1
Figure 4-6 Effective Beam and Slab Sections for Stiffness Ratio
α f (ACI 13.2.4)
 
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