Problem 10.12. Vibration of a steel-concrete composite floor -including beam’s weight

Take into consideration the beam’s mass, mb = 125 kg/m in the previous problem. Determine the modified eigenfrequency of the slab.
a) Approximate using the deflections of the beam and the slab.

Eq.(8-57)

b) Use Dunkerley’s approximation.

Stiffness of the simply supported beams are: EI = 6.42×105 kNm2. Stiffness of the isotropic plate is: Ds = 9.3 × 10 Nm2/m, mass of the plate is m = 540 kg/m2.

Solve Problem

Solve

Problem a)

Approximate eigenfrequency calculated from the deflecions, fn [Hz]=

Problem b)

Approximate eigenfrequency calculated by the summation theorems, fn [Hz]=

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Steps

Step by step

See Example 10.7.

Problem a)

Step 1. Determine the deflections of the beam and the slab.

Show deflections

The beam’s deflection is modified by the beam’s weight.

wb=5384mb+mbgLx4EI=5384(540×2.4+150)×9.81×8.046.42×108×103=1.16 mmws=1384mgb4D=5384540×9.81×2.449.3×106×103=4.92×106 m=0.0492 mm

The multispan slab is assumed to be a 1 m wide single span beam built-in at both ends.

Step 2. Approximate the eigenfrequency of the slab with the superposition of the above deflections.

Show eigenfrequency

Eq.(8-57).

w=wb+ws=1.16+0.0492=1.207 mmfn=18w=181.207=16.38 Hz

Problem b)

Step 1. Approximate eigenfrequency of the beam using Dunkerley’s theorem.

Show eigenfrequency

Approximate eigenfrequency of the hinged beam with two masses is

Eq.(10-102) and Table 8.3.

fx2=1f12+1f221=4mbLx4π2EI+4mbLx4π2EI1=π2EI4mb+mbLx4=   =π2×6.42×1084×540×2.4+150×8.04=272.2 1sec2

Step 2. Determine the eigenfrequency of the whole plate using Föppl’s approximation.

Show eigenfrequency

Eigenfrequency of the hinged slab:

Eq.(10-103).

fs2=π2D4mb4=π2×9.3×1064×540×2.44=1281 1sec2

In the relevant vibration mode both the beams and the plate undergo vibration as it is shown in the Figure.

The eigenfrequency is approximated by Föppl’s theorem. The edges of the slab is assumed to be built-in as the deformed shape shows.

fI2=1fx2+15.1fs21=1272.2+15.1×12811=224.51sec2fI=16.16 Hz

Results

Worked out solution

See Example 10.7.

Problem a)

The beam’s deflection is modified by the beam’s weight.

wb=5384mb+mbgLx4EI=5384(540×2.4+150)×9.81×8.046.42×108×103=1.16 mmws=1384mgb4D=5384540×9.81×2.449.3×106×103=4.92×106 m=0.0492 mm

The multispan slab is assumed to be a 1 m wide single span beam built-in at both ends.

Approximate eigenfrequency of the slab is given using the superposition of the above deflections.

Eq.(8-57).

w=wb+ws=1.16+0.0492=1.207 mmfn=18w=181.207=16.38 Hz

Problem b)

Approximate eigenfrequency of the hinged beam with two masses is

Eq.(10-102) and Table 8.3.

fx2=1f12+1f221=4mbLx4π2EI+4mbLx4π2EI1=π2EI4mb+mbLx4=   =π2×6.42×1084×540×2.4+150×8.04=272.2 1sec2

Eigenfrequency of the hinged slab:

Eq.(10-103).

fs2=π2D4mb4=π2×9.3×1064×540×2.44=1280.8 1sec2

In the relevant vibration mode both the beams and the plate undergo vibration as it is shown in the Figure.

The eigenfrequency is approximated by Föppl’s theorem. The edges of the slab is assumed to be built-in as the deformed shape shows.

fI2=1fx2+15.1fs21=1272.2+15.1×12811=224.51sec2fI=16.16 Hz