How to calculate natural frequency of a circular plate

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SUMMARY

The discussion focuses on measuring the natural frequency of a 170mm diameter, 10mm thick aluminum circular plate using a Data Physics analyzer. The user, Steve, reports a measured frequency of 1800 Hz, which significantly deviates from the theoretical calculation of 187.25 Hz based on the equation wn = B √(Et³/ρa⁴(1-ν)). Key parameters used in the calculation include Young's Modulus (E = 75 GPa), mass density (ρ = 2500 kg/m³), and Poisson's Ratio (ν = 0.33), with a configuration constant B of 6.09. The discrepancy is attributed to the method of striking the plate and the placement of the accelerometer.

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spggodd
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I am trying to get used to using a Data Physics analyzer at work in order to measure the natural frequency of components of a larger project I am involved in, my method described is intentionally crude as I was trying to do this as a quick play around before diving into the real thing..

To start off, I have found a aluminium circular plate component 170mm dia and 10mm thick. It has 7 small thru holes on a 160mm pcd and a 20mm circular boss at the centre of the plate, protruding 30mm on one side.

I have held the component by the central boss and hit it.
I am reading what I think is a natural frequency of 1800 Hz.

To compare, I tried to compare this to simple theory of a circular plate and found the following equation:

wn =B √(Et3/ρa4(1-ν))

Where:

E = Youngs Mondulus
I = Area Moment of Interia
a = Diameter of the Plate
ν = Poisons Ratio
ρ = Mass Density
B = Constant based on the configuration (Clamped at edge = 11.84, Free at edge = 6.09, Clamped at center = 4.35 and Hinged at edge = 5.90)

I used some general values for the aluminium (ρ=2500kg/m^3, E = 75 GPa, ν=0.33)
I took B = 6.09

I ended up with 187.25 Hz which is way below what I was expecting.

Can anyone spot why I'm so far out or can you advise if my method is not correct?

Many Thanks
Steve
 
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Also, the accelerometer I'm using is currently stuck down with duct tape on the outer edge of the component.

|----|
|...| <------- here
|...|
|...|
|...|
|...|
|...|--------|
|.....|
|----- - -----| - ----- - -----
|.....|
|...|--------|
|...|
|...|
|...|
|...|
|...|
|----|
 
I'm by no means an expert here at all but the only thing that jumps out to me is the position & force of the strike. Does that not need to be considered?
 

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