Problem 8.2. Additional mass – frequency of beam with hinged ends

Determine the concentrated mass that should be placed at the middle of a simply supported beam to reduce the fundamental frequency to the half of the original value
a) using approximated formula based on the deflection

Eq.(8-57)

b) using the summation theorem.
Bending stiffness of the beam is: EI = 6000 kNm2, distributed mass is: m = 60 kg/m, span is L = 6 m. 

Solve Problem

Solve

Problem a)

Additional mass, M [kg]=

Problem a)

Additional mass, M [kg]=

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Steps

Step by step

Problem a)

Step 1.  Calculate the maximum deflection of the beam with distributed mass only. Approximate natural frequency with the aid of the deflection. 

Show frequency, fm

See Table 3.5. and Eq.(8-57)
wm=5mgL4384EI=5×60×10×6.04384×6000×103103=1.69 mmfm=18wm=181.69=13.8 Hz

Step 2.  Applying superposition give the maximum deflection of the beam with the distributed and the additional concentrated masses. Approximate natural frequency with the aid of the deflection. 

Show frequency, fm+M

See Table 3.5. and Eq.(8-57)

wm+M=wm+MgL348 EIfm+M=18wm+M=18wm+MgL348 EI

Step 3.  Express additional mass, M from the equality fm+M = fm/2.

Show mass value

fm2= fm+M=18wm+MgL348EI      M=48EIgL32×18fm2wm=48×600010×6.032×1813.8521.69=675 kg

Problem b)

Step 1.  Calculate natural frequency of the beam with uniform mass only.

Show frequency, fm

Eq.(8-49)
fm=π2EI4mL4=π2×6000×1034×60×6.04=13.8 Hz

Step 2.  Write natural frequency of the beam with a concentrated mass only. 

Show frequency, fM

Eq.(8-15)

fM=12πkM=12π48EIML3 where   k=Pu=PPL348EI=48EIL3

Step 3.  Approximate fundamental frequency with Dunkerley’s summation theorem.

Show frequency, fM+m

See Table 8.3 and Eq.(8-58).
1fM+m2=1fm2+1fM2

Step 4.  Express additional mass, M from the equality fm+M = fm/2.

Show mass value

fm2=fm+M=1fm2+1fM2 0.5        4fm2=1fm2+1fM2      fM2=fm23=14π248EIML3   M=48EI4π2L33fm2=48×6000×10310×6.03313.82=532.2 kg

Note that the second solution gives more accurate result.

Results

Worked out solution

Problem a)

Maximum deflection of the beam with distributed mass only is 

See Table 3.5.
wm=5mgL4384EI=5×60×10×6.04384×6000×103103=1.69 mm

Its natural frequency can be approximated as:

Eq.(8-57)

fm=18wm=181.69=13.8 Hz

Applying superposition the maximum deflection of the beam with the distributed and the additional concentrated masses is also calculated. 

See Table 3.5.

wm+M=wm+MgL348 EI

The approximate natural frequency is:

fm+M=18wm+M=18wm+MgL348 EI

Additional mass, M is expressed from the equality fm+M = fm/2:

fm2= fm+M=18wm+MgL348EI      M=48EIgL32×18fm2wm=48×600010×6.032×1813.8521.69=675 kg

Problem b)

Natural frequency of the beam with uniform mass only is the following:

Eq.(8-49)
fm=π2EI4mL4=π2×6000×1034×60×6.04=13.8 Hz

Natural frequency of the beam with a concentrated mass only is

Eq.(8-15)

fM=12πkM=12π48EIML3 where   k=Pu=PPL348EI=48EIL3

The fundamental frequency is approximated by Dunkerley’s summation theorem.

See Table 8.3 and Eq.(8-58).
1fM+m2=1fm2+1fM2

Additional mass, M is expressed from the equality fm+M = fm/2.

fm2=fm+M=1fm2+1fM2 0.5        4fm2=1fm2+1fM2      fM2=fm23=14π248EIML3   M=48EI4π2L33fm2=48×6000×10310×6.03313.82=532.2 kg

Note that the second solution gives more accurate result.