Page Comparison

h1. What values should I use for mass\- and stiffness-proportional damping coefficients?

*Answer:* Mass\- and stiffness-proportional [damping|kb:Damping], normally referred to as Rayleigh damping, is commonly used in [nonlinear-dynamic|kb:Nonlinear] analysis. Suitability for an incremental approach to numerical solution merits its use. During formulation, the damping matrix is assumed to be proportional to the mass and stiffness matrices as follows:

!fig 1.png|align=center,border=0!

where

* \*{math}\eta{math}\* is the mass-proportional damping coefficient; and

* \*{math}\delta{math}\* is the stiffness-proportional damping coefficient.

Relationships between the modal equations and orthogonality conditions allow this equation to be rewritten as:

!Figure 1.png|align=center,border=0!

where

* \*{math}\xi_n{math}\* is the critical-damping ratio; and

* \*{math}\omega_n{math}\* is the natural frequency ({math}\omega_n = 2 \pi f_n{math}).

Here, it can be seen that the critical-damping ratio varies with natural frequency. The values of *{math}\eta{math}\* and *{math}\delta{math}\* are usually selected, according to engineering judgement, such that the critical-damping ratio is given at two known frequencies. For example, 5% damping ( *{math}\xi{math}\* = 0.05 ) at the first natural frequency of the structure ( *{math}\omega_i{math}\* =  *{math}\omega_1{math}\* ), and at *{math}\omega_j{math}\* = 188.5 (30 Hz). According to the equation above, the critical-damping ratio will be smaller between these two frequencies, and larger outside.

If the damping ratios ( *{math}\xi_i{math}\* and *{math}\xi_j{math}\* ) associated with two specific frequencies ( *{math}\omega_i{math}\* and *{math}\omega_j{math}\* ), or modes, are known, the two Rayleigh damping factors ( *{math}\eta{math}\* and *{math}\delta{math}\* ) can be evaluated by the solution of a pair of simultaneous equations, given mathematically by:

!Figure 2.png|align=center,border=0!

[SAP2000|sap2000:home] allows users to either specify coefficients *{math}\eta{math}\* and *{math}\delta{math}\* directly, or in terms of the critical-damping ratio at two different frequencies, *f* (Hz), or periods, *T* (sec).

When damping is set to equal for both frequencies, the conditions associated with the proportionality factors simplify as follows:

!Figure 3.png|align=center,border=0!


h1. References

* Wilson, Dr. Edward L. _Static & Dynamic analysis of Structures_. 4th ed. Berkeley: Computers and Structures, Inc., 2004.
Print.
Available for purchase on the {new-tab-link:http://www.csiberkeley.com/}CSI{new-tab-link} Products > {new-tab-link:http://orders.csiberkeley.com/ProductDetails.asp?ProductCode=ELWDOC-3D}Books{new-tab-link} page {new-tab-link:http://orders.csiberkeley.com/ProductDetails.asp?ProductCode=ELWDOC-3D}Books{new-tab-link} [http://orders.csiberkeley.com/ProductDetailsSearchResults.asp?ProductCode=ELWDOC-3D]Cat=2