Eigenfunctions for a Uniform Free Beam
Introduction
We show here how to find the eigenfunction for a beam with free edge conditions.
Equations
We can find a the eigenfunction which satisfy
[math]\displaystyle{ \partial_x^4 w_n = \lambda_n^4 w_n \,\,\, -L \leq x \leq L }[/math]
plus the edge conditions of zero bending moment and shear stress
Solution
General solution of the differential equation is :
[math]\displaystyle{ w_n(x) = C_1 \sin(\lambda_n x) + C_2 \cos(\lambda_n x) + C_3 \sinh(\lambda_n x) + C_4 \cosh(\lambda_n x)\, }[/math]
Due to symmetry of the problem, dry natural vibrations of a free beam can be split into two different sets of modes, symmetric (even) modes and skew-symmetric (odd) modes.
Symmetric modes
[math]\displaystyle{ C_1 = C_3 = 0 \Rightarrow w_n(x) = C_2 \cos(\lambda_n x) + C_4 \cosh(\lambda_n x) }[/math]
By imposing boundary conditions at [math]\displaystyle{ x = L }[/math] :
[math]\displaystyle{ \begin{bmatrix} - \cos(\lambda_n L)&\cosh(\lambda_n L)\\ \sin(\lambda_n L)&\sinh(\lambda_n L)\\ \end{bmatrix} \begin{bmatrix} C_2\\ C_4\\ \end{bmatrix} = \begin{bmatrix} 0\\ 0\\ \end{bmatrix} }[/math]
For a nontrivial solution one gets:
[math]\displaystyle{ \tan(\lambda_n L)+\tanh(\lambda_n L)=0\, }[/math]
The first three roots are :
[math]\displaystyle{ \lambda_0 L = 0, \lambda_2 L = 2.365, \lambda_4 L = 5.497\, }[/math]
Symmetric natural modes can be written in normalized form as :
[math]\displaystyle{ w_n(x) = \frac{1}{2}\left( \frac{\cos(\lambda_n x)}{\cos(\lambda_n L)}+\frac{\cosh(\lambda_n x)}{\cosh(\lambda_n L)} \right ) }[/math]
Anti-symmetric modes
[math]\displaystyle{ C_2 = C_4 = 0 \Rightarrow w_n(x) = C_1 \sin(\lambda_n x) + C_3 \sinh(\lambda_n x) }[/math]
By imposing boundary conditions at [math]\displaystyle{ x = l }[/math] :
[math]\displaystyle{ \begin{bmatrix} - \sin(\lambda_n L)&\sinh(\lambda_n L)\\ -\cos(\lambda_n L)&\cosh(\lambda_n L)\\ \end{bmatrix} \begin{bmatrix} C_1\\ C_3\\ \end{bmatrix} = \begin{bmatrix} 0\\ 0\\ \end{bmatrix} }[/math]
For a nontrivial solution one gets:
[math]\displaystyle{ -\tan(\lambda_n L)+\tanh(\lambda_n L)=0\, }[/math]
The first three roots are :
[math]\displaystyle{ \lambda_1 L = 0, \lambda_3 L = 3.925, \lambda_5 L = 7.068\, }[/math]
Anti-symmetric natural modes can be written in normalized form as :
[math]\displaystyle{ w_n(x) = \frac{1}{2}\left( \frac{\sin(\lambda_n x)}{\sin(\lambda_n L)}+\frac{\sinh(\lambda_n x)}{\sinh(\lambda_n L)} \right ) }[/math]
The anti-symmetric modes can be nomalised so that their inner products equal the Kronecker delta by letting :
[math]\displaystyle{ w_n(x) = C_3\left( \sinh(\lambda_n L)\sin(\lambda_n x) + \sin(\lambda_n L)\sinh(\lambda_n x) \right ) }[/math]
where :
[math]\displaystyle{ C_3 = \sqrt(2 \lambda_n))/\sqrt(\lambda_n L (-2 + \cos(2 \lambda_n L) + \cosh(2 \lambda_n L)) - 3 (\sinh(\lambda_n L))^2 \sin(2 \lambda_n L) + 3 (sin(\lambda_n L))^2 \sinh(2 \lambda_n L)); }[/math]
Natural Frequencies
The equation in the time domain for a beam is
[math]\displaystyle{ m\partial_t^2 w + EI \partial_x^4 w = 0 }[/math]
so that, having obtained eigenvalues [math]\displaystyle{ \lambda_n }[/math], the natural frequency can be readily calculated :
[math]\displaystyle{ \omega_n = \lambda_n^2 \sqrt\frac{EI}{m} }[/math]