Single degree of freedom damped free vibrations: Difference between revisions

From StructuralWiki
Jump to navigation Jump to search
Line 89: Line 89:
|-
|-
| width = "50px" |
| width = "50px" |
| <tex>\lambda_{1,2} = - \xi \omega \pm \sqrt{(\xi \omega)^2 - \omega^2} = - \xi \omega \pm \omega i \sqrt{1 - \omega}</tex>
| <tex>\lambda_{1,2} = - \xi \omega \pm \sqrt{(\xi \omega)^2 - \omega^2} = - \xi \omega \pm \omega i \sqrt{1 - \xi^2}</tex>
| align = "right" | (8)
| align = "right" | (8)
|}
|}
where
{| width="100%"
|-
| width = "50px" |
| <tex>\omega_D \equiv \omega \sqrt{1 - \xi^2} </tex>
| align = "right" | (9)
|}
is the free vibration frequency of damped system.


=== Overcritically-Damped Systems ===
=== Overcritically-Damped Systems ===

Revision as of 03:29, 6 October 2009

Governing Equation

Governing equation for the motion of single of freedom oscilator can be written as:


<tex>m\ddot{u}(t) + c\dot{u}(t) + ku(t) = 0</tex> (1)


This is a second-order linear ordinary differential equation with constant coefficients that can be rearranged as follows:


<tex>\ddot{u}(t) + \frac{c}{m}\dot{u}(t) + \frac{k}{m}u(t) = 0</tex> (2)


After substitution of <tex>\omega = \sqrt{\frac{k}{m}}</tex> Eqn. (2) becomes


<tex>\ddot{u}(t) + \frac{c}{m} \dot{u}(t) + \omega^2 u(t) = 0</tex> (3)


which yields the following characteristic equation


<tex>\lambda^2 + \frac{c}{m} \lambda + \omega^2 = 0</tex> (4)


with a solution


<tex>\lambda_{1,2} = \frac{-\frac{c}{m} \pm \sqrt{(\frac{c}{m})^2 - 4 \omega^2}}{2} = -\frac{c}{2m} \pm \sqrt{(\frac{c}{2m})^2 - \omega^2}</tex> (5)


Critically-Damped Systems

If the radical term in Eqn. (5)is set equal to zero then <tex>c/2m = \omega</tex> and the critical value of damping coefficient, <tex>c_c</tex> can be expressed as


<tex>c_c = 2 m \omega</tex> (6)


Undercritically-Damped Systems

If damping is less than critical, i.e. if <tex>c < c_c</tex> (in other words if <tex>c < 2 m \omega</tex>), it is convenient to define the damping in the terms of damping ratio, which is defined as


<tex>\xi = \frac{c}{c_c} = \frac{c}{2 m \omega}</tex> (7)


Introducing <tex>\xi</tex> into Eq. (5) yields


<tex>\lambda_{1,2} = - \xi \omega \pm \sqrt{(\xi \omega)^2 - \omega^2} = - \xi \omega \pm \omega i \sqrt{1 - \xi^2}</tex> (8)


where


<tex>\omega_D \equiv \omega \sqrt{1 - \xi^2} </tex> (9)


is the free vibration frequency of damped system.

Overcritically-Damped Systems

Derivation

       To Do: Provide solution for single degree of freedom damped free vibrations (who: user:ok; priority: 100; hours: 0) (all) (cat)

References

  • Ray W. Clough and Joseph Penzien: Dynamics of Structures, 2nd edition, McGraw-Hill, New York, 1993. 738 pages. ISBN 0-07-011394-7, section 2-6, p. 26

External Links

 

Home > Topics > Dynamics e
Overview Overview  · Notation  · Flutter
Single Degree of Freedom Damped Free Vibrations

Related Categories Dynamics