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

Click For Summary
SUMMARY

The discussion focuses on calculating the natural frequency of a cantilever beam that is tapered in breadth with a uniform thickness. The beam is clamped at one end, with a constant length (L) and thickness (H), while the breadth (B) varies along its length based on the angle from the z-axis. The solution involves modeling the beam as a massless system with a point mass at the end, applying the formula for fundamental frequency, ω = √(k/m), and utilizing Bessel functions for the derivation of vibration formulas specific to disks with a central hole.

PREREQUISITES
  • Understanding of cantilever beam theory
  • Familiarity with natural frequency calculations
  • Knowledge of Bessel functions and their applications
  • Proficiency in MATLAB for plotting and analysis
NEXT STEPS
  • Research the derivation of vibration formulas for disks with holes
  • Learn about the application of Bessel functions in mechanical systems
  • Explore MATLAB functions for plotting frequency vs. angle
  • Study the impact of Poisson's ratio on beam theory
USEFUL FOR

Mechanical engineers, structural analysts, and students involved in vibration analysis and beam theory who are looking to understand the dynamics of tapered cantilever beams.

jazzkiwi
Messages
1
Reaction score
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
 
Engineering news on Phys.org
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 \omega = \sqrt{\frac{k}{m}}
 
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.
 

Similar threads

Replies
6
Views
8K
  • · Replies 7 ·
Replies
7
Views
3K
Replies
7
Views
24K
  • · Replies 3 ·
Replies
3
Views
7K
  • · Replies 1 ·
Replies
1
Views
2K
Replies
1
Views
6K
  • · Replies 3 ·
Replies
3
Views
41K
Replies
4
Views
20K
  • · Replies 4 ·
Replies
4
Views
8K
  • · Replies 1 ·
Replies
1
Views
1K