Difference between revisions of "Template:Equations for a beam"

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by the following
 
by the following
 
<center><math>
 
<center><math>
\partial_x^2\left(D\partial_x^2 \zeta\right) + \rho_i h \partial_t^2 \zeta = p
+
\partial_x^2\left(D(x)\partial_x^2 \zeta\right) + \rho_i h(x) \partial_t^2 \zeta = p
 
</math></center>
 
</math></center>
 
where <math>D</math> is the flexural rigidity, <math>\rho_i</math> is the density of the plate,
 
where <math>D</math> is the flexural rigidity, <math>\rho_i</math> is the density of the plate,

Revision as of 07:14, 4 April 2009

There are various beam theories that can be used to describe the motion of the beam. The simplest theory is the Bernoulli-Euler Beam theory (other beam theories include the Timoshenko Beam theory and Reddy-Bickford Beam theory where shear deformation of higher order is considered). For a Bernoulli-Euler Beam, the equation of motion is given by the following

[math]\displaystyle{ \partial_x^2\left(D(x)\partial_x^2 \zeta\right) + \rho_i h(x) \partial_t^2 \zeta = p }[/math]

where [math]\displaystyle{ D }[/math] is the flexural rigidity, [math]\displaystyle{ \rho_i }[/math] is the density of the plate, [math]\displaystyle{ h }[/math] is the thickness of the plate, [math]\displaystyle{ p }[/math] is the pressure and [math]\displaystyle{ \zeta }[/math] is the plate vertical displacement. Note that this equations simplifies if the plate has constant properties.

The edges of the plate can satisfy a range of boundary conditions. The natural boundary condition (i.e. free-edge boundary conditions).

[math]\displaystyle{ \partial_x^2 \zeta = 0, \,\,\partial_x^3 \zeta = 0 }[/math]

at the edges of the plate.