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Structural dynamics and vibration testing

Rayleigh stiffness coefficient from two target frequencies

Stiffness-proportional Rayleigh coefficient β that gives chosen damping ratios at two chosen frequencies.

Ref
SDY-40
Rev
v1
Field
Structural dynamics and vibration testing
Result
β [s]

The stiffness coefficient is β = 2(ζ₂ω₂ − ζ₁ω₁)/(ω₂² − ω₁²). For equal targets this is β = 2ζ/(ω₁ + ω₂). Together with α it gives exactly the two target damping ratios at the two target frequencies and a smooth curve between and beyond them. The stiffness term raises damping at high frequency, and can over-damp modes above ω₂.

Stiffness-proportional Rayleigh coefficient β that gives chosen damping ratios at two chosen frequencies. It is the second row of the two-frequency calibration.

Calculator

Solve for
s
rad/s
235
0.0050.2
rad/s
15200
0.0050.2
  • Mass coefficient α0.8 1/s
  • Damping at twice the upper target frequency0.085
  • Frequency of minimum damping, √(α/β)20 rad/s

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Stiffness coefficient (s) current value 0.002 s
ζ2Damping ratio at ω₂Key driver
−4e-40.01
ω2Upper target angular frequency
4.76e-40.004
ζ1Damping ratio at ω₁
00.0026
ω1Lower target angular frequency
0.001330.00238
  • The two targets give β = 0.002 s; at twice the upper frequency the damping is already 8.5 %.
  • A stiffness coefficient that is too large damps high modes heavily and may force a smaller time step in explicit analysis.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (s)Local stepChange in result
ζ2 Damping ratio at ω₂0.005 to 0.2 −4e-40.010.0104+10%+13.3 %
ω2 Upper target angular frequency15 to 200 rad/s4.762e-40.0040.003524+10%−7.41 %
ζ1 Damping ratio at ω₁0.005 to 0.2 00.00260.0026+10%−3.33 %
ω1 Lower target angular frequency2 to 35 rad/s0.0013330.0023810.001048+10%−1.96 %

Sweep of Damping ratio at ω₂

Damping ratio at ω₂Stiffness coefficient (s)
0.005−4e-4
0.029389e-4
0.053750.0022
0.078130.0035
0.10250.0048
0.12690.0061
0.15120.0074
0.17560.0087
0.20.01

Sweep one variable

Stiffness coefficient (s)Hover, touch, or use the arrow keys on the chart
00.0020.0040.0060.0080.01 0.050.10.150.2 Damping ratio at ω₂ now 0.002

Variables and how each one contributes

β

Stiffness coefficient

Result · s

What the equation gives you. Everything else feeds it.

ω1

Lower target angular frequency

rad/s · typical 2 to 35

The lower target angular frequency, in rad/s. Changes where the damping is pinned down. Raising it by 10 % (to 11) moves the result by −1.96 %, from 0.002 to 0.001961 s.

ζ1

Damping ratio at ω₁

· typical 0.005 to 0.2

The target damping ratio at the lower frequency. Raises the coefficient that sets the low-frequency damping. Raising it by 10 % (to 0.055) moves the result by −3.33 %, from 0.002 to 0.001933 s.

ω2

Upper target angular frequency

rad/s · typical 15 to 200

The upper target angular frequency, in rad/s. It must be larger than the lower one. Changes where the damping is pinned down. Raising it by 10 % (to 44) moves the result by −7.41 %, from 0.002 to 0.001852 s.

ζ2

Damping ratio at ω₂

· typical 0.005 to 0.2

The target damping ratio at the upper frequency. Raises the coefficient that sets the high-frequency damping. Raising it by 10 % (to 0.055) moves the result by +13.3 %, from 0.002 to 0.002267 s.

Worked example with the values above

  1. Numerator: 2(ζ₂ω₂ − ζ₁ω₁) = 2 × (2 − 0.5) = 3.
  2. Denominator: ω₂² − ω₁² = 1,500.
  3. β = 0.002 s.

Assumptions and limits

  • Classical damping in the form C = αM + βK, with α and β constant.
  • The two target frequencies are distinct and positive, and the damping between them is accepted to dip below the targets.

Common mistakes

  • Assuming Rayleigh damping holds the target ratio across the band: it dips between the two targets and rises sharply outside them.
  • Mixing α in 1/s with a frequency in Hz.
  • Choosing target frequencies that do not bracket the modes that matter.

Statistics and uncertainty

The calibration is exact for the two chosen points, but the damping in between and outside them is a model result and not a measurement. Check it against measured modal damping across the band.

Where it is used

  • Setting damping in transient and modal finite-element analyses from two measured damping ratios.
  • Checking the predicted damping of every mode in a band after calibration.

Maths you need

  • Damping matrix: C in M ü + C u̇ + K u = F
  • Modal damping ratio: damping of a single mode as a fraction of critical

Related formulas

Practise this formula