What values should I use for mass- and stiffness-proportional damping coefficients?
Answer: Mass- and stiffness-proportional damping, normally referred to as Rayleigh damping, is commonly used in nonlinear-dynamic 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:
where
- *
Unknown macro: {math}* is the mass-proportional damping coefficient; and
\eta
- *
Unknown macro: {math}* is the stiffness-proportional damping coefficient.
\delta
Relationships between the modal equations and orthogonality conditions allow this equation to be rewritten as:
where
- *
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\xi_n
- *
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\omega_n
Unknown macro: {math}).\omega_n = 2 \pi f_n
Here, it can be seen that the critical-damping ratio varies with natural frequency. The values of *
\eta
* and *
\delta
* are usually selected, according to engineering judgement, such that the critical-damping ratio is given at two known frequencies. For example, 5% damping (*
\xi
* = 0.05 ) at the first natural frequency of the structure ( *
\omega_i
* = *
\omega_1
* ), and at *
\omega_j
* = 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 ( *
\xi_i
* and *
\xi_j
* ) associated with two specific frequencies ( *
\omega_i
* and *
\omega_j
* ), or modes, are known, the two Rayleigh damping factors ( *
\eta
* and *
\delta
* ) can be evaluated by the solution of a pair of simultaneous equations, given mathematically by:
SAP2000 allows users to either specify coefficients *
\eta
* and *
\delta
* 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:
References
- Wilson, Dr. Edward L. Static & Dynamic analysis of Structures. 4th ed. Berkeley: Computers and Structures, Inc., 2004. Print. (Stiffness and Mass Proportional Damping, page 231)
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