Single degree of freedom damped free vibrations: Difference between revisions

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== Governing Equation ==
== Governing Equation ==


<tex>m\ddot{u}(t) + c\dot{u}(t) + ku(t) = 0</tex>
Governing equation for the motion of single of freedom oscilator can be written as:




This is a [[second-order linear ordinary differential equation with constant coefficients]] that yields the following solution:
{| width="100%"
|-
| width = "50px" |
| <tex>m\ddot{u}(t) + c\dot{u}(t) + ku(t) = 0</tex>
| align = "right" | (1)
|}
 
 
This is a [[second-order linear ordinary differential equation with constant coefficients]] that can be rearranged as follows:
 
 
{| width="100%"
|-
| width = "50px" |
| <tex>\ddot{u}(t) + \frac{c}{m}\dot{u}(t) + \frac{k}{m}u(t) = 0</tex>
| align = "right" | (2)
|}
 
 
After substitution of <tex>\omega = \sqrt{\frac{k}{m}}</tex> (Eqn. 2) becomes
 
 
{| width="100%"
|-
| width = "50px" |
| <tex>\ddot{u}(t) + \frac{c}{m} \dot{u}(t) + \omega^2 u(t) = 0</tex>
| align = "right" | (3)
|}
 
 
which yields the following [[characteristic equation]]
 
 
{| width="100%"
|-
| width = "50px" |
| <tex>\lambda^2 + \frac{c}{m} \lambda + \omega^2  = 0</tex>
| align = "right" | (3)
|}
 
 
with a solution
 
 
{| width="100%"
|-
| width = "50px" |
| <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>
| align = "right" | (3)
|}
 
 
=== Critically-Damped Systems ===
 
=== Undercritically-Damped Systems ===
 
=== Overcritically-Damped Systems ===
 
== Derivation ==


{{To Do | who = user:ok | comment = Provide solution for single degree of freedom damped free vibrations}}
{{To Do | who = user:ok | comment = Provide solution for single degree of freedom damped free vibrations}}

Revision as of 03:02, 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> (3)


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> (3)


Critically-Damped Systems

Undercritically-Damped Systems

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

 

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