What makes a structure amplify an input? Why does damping matter? Start with one mass, one spring and one damper, then connect the response to real measurement questions.
Try “Near resonance”, then increase damping. Move above √2 × the natural frequency to explore isolation.
Selected damping5% reference● Current excitation
Steady-state motion
Slowed to 0.5 cycles/s. Both motions share a display scale that adjusts to fit; their amplitude ratio and phase are preserved.
Natural frequency—
Frequency ratio—
Response / base—
Response phase—
Use the controls to explore the response of a linear spring–mass–damper system.
The model behind the motion
One mode. A useful starting point.
The base displacement is y(t); the mass displacement in a fixed reference frame is x(t). The spring and damper react to their relative motion.
mx¨+c(x˙−y˙)+k(x−y)=0
fn=2π1mk,ζ=2kmc,r=fnf
YX=1−r2+i2ζr1+i2ζr
The chart shows the magnitude of this complex ratio; phase describes the timing of the response relative to the base. For a single harmonic frequency, the same ratio applies to absolute acceleration amplitudes.
Same input RMS. Different structural response.
Random-vibration response explorer
Both inputs contain the same total acceleration variance. Spectrum A concentrates energy near 80 Hz; spectrum B near 250 Hz. Move the structural mode between them and compare the predicted absolute acceleration response.
A · Low-frequency emphasisB · High-frequency emphasisNatural frequency
01 / Base acceleration PSD
Equal area in linear Hz gives equal input RMS.
02 / Absolute response PSD
The transfer function weights each frequency differently.
Both axes are logarithmic. Each chart scales its PSD axis independently; compare the axis values as well as the curve shapes.
H is the absolute-acceleration transfer function of the same linear, viscously damped, base-excited SDOF model used above. These are stationary, zero-mean inputs with one-sided PSDs. The two spectra are alternative tests, not simultaneous inputs.
Each synthetic profile has a small flat background plus a Gaussian-shaped emphasis: A is centred at 80 Hz with a 20 Hz width parameter; B at 250 Hz with a 45 Hz width parameter. Both are normalized to the selected RMS over 20–500 Hz and are zero outside that band. The input profiles stay fixed when you move the mode.
Response variance is integrated in linear frequency using trapezoidal integration at 0.1 Hz spacing. RMS is the square root of variance; the area under a curve on logarithmic screen coordinates is not the variance.
This predicts acceleration, not stress, fatigue damage or a qualification verdict. Multiple modes, nonlinear behaviour and other response quantities require their own models.
Displace a mass attached to a spring and release it. Mass stores kinetic energy; the spring stores elastic energy. Their balance sets the natural frequency. More stiffness raises it; more mass lowers it. With damping, the oscillation decays.
A shaker supplies continuous excitation. The steady-state response depends on excitation frequency relative to the natural frequency, as well as damping. Near resonance, even a modest base motion can produce a much larger response.
Damping dissipates energy and reduces the resonant peak. For harmonic base excitation, it can also increase transmitted motion well above resonance. In this linear model, absolute-motion isolation starts above a frequency ratio of √2.
Yes. Overall RMS describes the integrated input spectrum, but not where its energy lies in frequency. Response depends on the input PSD weighted by the squared magnitude of the relevant transfer function. Energy close to a lightly damped mode can contribute strongly.
A transient excites systems differently depending on pulse shape, duration and natural frequency. A shock response spectrum reports peak responses of a family of oscillators at a stated damping. It does not uniquely reconstruct the original time history.
An FFT peak identifies signal content. Calling it a structural mode requires more evidence about the excitation and the system response. Likewise, a shift between resonance searches calls for checking setup repeatability and environmental conditions before drawing a conclusion about structural change.
The SDOF response, transmissibility and shock explanations follow the analytical framework in Tom Irvine’s An Introduction to Shock and Vibration Response Spectra. Visit Tom Irvine’s Vibrationdata reference library (external website) for further reading.