Cantilever Beam, Tapered in breadth, uniform thickness, natural frequency

In summary, the conversation discusses finding the natural frequency of a Cantilever Beam with a tapered breadth and uniform thickness. The end goal is to find an equation for frequency as a function of the angle of the side cut, which will be used in MATLAB for a plot. One idea mentioned is to find an equivalent system of a massless beam with a point mass at the end and use the stiffness and point mass to calculate the fundamental frequency. Another suggestion is to use formulas for vibration of disks, with adjustments for the hole in the middle. It is also noted that Poisson's ratio should be set to 0 for this solution.
  • #1
jazzkiwi
1
0
Hey there
I need to find the natural frequency of a Cantilever Beam. The beam is tapered in breadth, but has a uniform thickness. So basically the end goal is an equation for f as a function of the angle of the side cut.

Clamped at one end
L=constant
B=changes though the length of the beam and is dependent on the angle from the z axis (along the beam)
H=constant (thickness)
E constant,
So obviously the second moment of area will be a function of x or angle.

The end equation will be used in MATLAB to for a plot angle vs frequency

Any pointers, or a solution would be most helpful,
Thanks for your time
 
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  • #2
Just an incomplete idea -

Find an equivalent system of a massless beam with a point mass at the end. Then use the stiffness of the beam, and the point mass as a simple spring-mass system and get the fundamental frequency from [tex]\omega = \sqrt{\frac{k}{m}}[/tex]
 
  • #3
If I understood your description correctly, your "beam" is the same shape as a slice cut out of a circular disk with a hole in the middle.

Formulas for the vibration of disks are well known, though you might have to find the derivations and extend them yourself to the case with a hole in the middle. The math involves Bessel functions.

You would need to take Poisson's ratio = 0, so there would be no circumferential strain in the solution for the full disk, and cutting it into "slices" would not make any difference. The simplest beam theories don't depend on Poisson's ratio at all, so this should work out OK.
 

Related to Cantilever Beam, Tapered in breadth, uniform thickness, natural frequency

1. What is a cantilever beam?

A cantilever beam is a type of structural element that is supported at only one end, with the other end hanging freely. It is commonly used in engineering and construction to support loads and resist bending forces.

2. What does it mean for a cantilever beam to be tapered in breadth?

A tapered cantilever beam is one that gradually decreases in width from its base to its free end. This design allows for a more efficient distribution of stress and can increase the strength and stiffness of the beam.

3. What is the significance of uniform thickness in a cantilever beam?

Uniform thickness in a cantilever beam means that the width of the beam remains constant from its base to its free end. This is important because it helps to evenly distribute stress and prevent weak points in the beam.

4. What is the natural frequency of a cantilever beam?

The natural frequency of a cantilever beam is the frequency at which it will vibrate when excited by an external force. This frequency is determined by the material properties, dimensions, and boundary conditions of the beam.

5. How can the natural frequency of a tapered cantilever beam be calculated?

The natural frequency of a tapered cantilever beam can be calculated using complex mathematical equations that take into account the material properties, dimensions, and boundary conditions of the beam. Alternatively, it can be determined experimentally by measuring the actual vibration frequency of the beam.

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