Kinematics of Euler Bernoulli and Timoshenko Beam Elements

In summary, Euler beam theory is appropriate when the length/depth of the beam is greater than 10, while Timoshenko beam theory is appropriate for beams with significant shear flexibility.
  • #1
bugatti79
794
1
Folks,

Trying to get some appreciation for what is going on in the attached schematic of 1)Euler bernoulli and 2) Timoshenko beam elements.

For the first one, ie the top picture, how was ##u- z \frac{dw}{dx}## arrived at?

thanks
 

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  • #2
dw/dx is the slope of the beam, which is assumed to be small. So dw/dx is also the angle the beam has rotated, in radians.

The top picture (Euler beam theory) assumes that cross sections of the beam stay perpendicular to the neutral axis. So the angle between a cross section and the vertical is the same as the slope of the beam.

The picture is (stupidly, IMHO) drawn with a "left handed" coordinate system (z and w positive downwards not upwards) which is where the minus signs come from.

In the bottom picture (Timoshenko beam theory) plane sections of the beam do not stay perpendicular to the neutral axis, so there is an extra shear strain (measured by angle gamma) involved.
 
  • #3
AlephZero said:
dw/dx is the slope of the beam, which is assumed to be small. So dw/dx is also the angle the beam has rotated, in radians.
Ok

AlephZero said:
The top picture (Euler beam theory) assumes that cross sections of the beam stay perpendicular to the neutral axis. So the angle between a cross section and the vertical is the same as the slope of the beam.
I understand this.

AlephZero said:
The picture is (stupidly, IMHO) drawn with a "left handed" coordinate system (z and w positive downwards not upwards) which is where the minus signs come from.
Ok, how does the ##z\frac{dw}{dx}## come about? Is this equivalent to Z times the cos of the angle?

AlephZero said:
In the bottom picture (Timoshenko beam theory) plane sections of the beam do not stay perpendicular to the neutral axis, so there is an extra shear strain (measured by angle gamma) involved.
Thanks
 
  • #4
bugatti79 said:
Ok, how does the ##z\frac{dw}{dx}## come about? Is this equivalent to Z times the cos of the angle?

dw/dx is the sine of the angle (sin θ = θ for small angles) but you are right about the basic idea.
 
  • #5
What practical examples are there where one shouldn't use Euler-Bernouilli to track beam deflection etc. Would it for applications of plastic loading?

Thanks
 
  • #6
bugatti79 said:
What practical examples are there where one shouldn't use Euler-Bernouilli to track beam deflection etc.

When the flexibility in shear is significant compared with the flexibility in pure bending.

For a rectangular section beam, Euler is OK when length/depth > 10 (some people say > 20).

For a more complicated criss sections, and/or composite beams made from several materials, you have to consider each case on its own merits.

With computer software like finite element analysis, you might as wel always use the Timoshenko formulation. Even if the correction is neglibile, it doesn't cause any numerical problems to include it.
 

1. What is the difference between Euler-Bernoulli and Timoshenko beam elements?

Euler-Bernoulli beam elements assume that the cross-sections of the beam remain perpendicular to the neutral axis during bending, while Timoshenko beam elements account for shearing deformation of the cross-sections. This makes Timoshenko beam elements more accurate for beams with high shear forces.

2. How do beam elements handle boundary conditions?

Beam elements use nodal displacements and rotations to represent boundary conditions. These are typically prescribed at the ends of the beam and are used to solve for the unknown nodal forces and moments.

3. What are the limitations of using beam elements?

Beam elements are only accurate for slender beams with small deformations. They also assume linear elastic behavior and do not account for material nonlinearity.

4. How are the stiffness and mass matrices calculated for beam elements?

The stiffness and mass matrices for beam elements are calculated using numerical integration techniques, such as the Gauss-Legendre quadrature method. These matrices are then assembled into the global stiffness and mass matrices for the entire beam structure.

5. Can beam elements be used for 3D structures?

No, beam elements are only applicable for 1D structures. For 3D structures, other types of finite elements, such as shell or solid elements, must be used. However, beam elements can be used as part of a 3D structural model by combining them with other element types.

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