Difference between revisions of "Template:Equations for a beam"
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+ | :<math> \zeta(x,0)=f(x) \,\! </math> | ||
+ | :<math> \frac{\partial \zeta(x,0)}{\partial t}=g(x) </math></center> |
Revision as of 08:25, 7 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
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).
at the edges of the plate.
The problem is subject to the initial conditions
- [math]\displaystyle{ \zeta(x,0)=f(x) \,\! }[/math]
- [math]\displaystyle{ \frac{\partial \zeta(x,0)}{\partial t}=g(x) }[/math]