Analysis of Structural Vibrations

 

Newton’s equation of motion for a rigid body states:

 

For a structure, the resultant of inertial forces are balanced by the resultant of elastic deformation forces.  The equation of motion for a structure is:

                                        (1)

where M is the structure dynamical matrix and K is the structure stiffness matrix.

 

Equation 1 has a solution of the type:

 

Substitute for x in Equation 1:

 

Arrange in standard eignenvalue form:

                                    (2)

or

                                  (3)

where Equation 2 is for M non-singular while Equation 3 is for K semi-definite.

 

Put in standard eigenvalue form:

 

 

Results in:

                       (4)

 is in general not symmetric even though K and M are symmetric.

Let  where L is the Cholesky factor of M.

Replace M in Equation 3 with its Cholesky factors:

 

 

Let

 

Whence:

 

 

 

 

 

                            (5)

Equation 5 is the symmetric form of Equation 4.  Equation 5 can now be solved for eigenvalues

 

 

The fundamental frequency of vibration of the structure is given by: