Resonance: Peak Response at the Natural Frequency

April 12, 2026

Problem

Drive a damped oscillator at various frequencies. Show that the amplitude peaks sharply at the natural frequency.

Explanation

A driven, damped harmonic oscillator responds most strongly when the driving frequency matches its natural frequency ω0\omega_0. This phenomenon is called resonance, and it's behind everything from singers shattering wine glasses to the Tacoma Narrows Bridge collapse.

The Setup

A mass-spring system with damping coefficient γ\gamma and natural frequency ω0=k/m\omega_0 = \sqrt{k/m}, driven by a sinusoidal force Fsin(ωt)F\sin(\omega t), has a steady-state response amplitude:

A(ω)=F/m(ω02ω2)2+(γω)2A(\omega) = \dfrac{F/m}{\sqrt{(\omega_0^{2} - \omega^{2})^{2} + (\gamma\omega)^{2}}}

This is a Lorentzian-like peak in ω\omega, centered near ω0\omega_0. The width of the peak depends on the damping: small damping gives a tall, narrow peak; large damping gives a short, broad one.

Step-by-Step Solution

Given: A driven oscillator with ω0=5  rad/s\omega_0 = 5\;\text{rad/s}, γ=0.5  s1\gamma = 0.5\;\text{s}^{-1}, and unit driving amplitude F/m=1F/m = 1.

Find: The response amplitude at ω=3\omega = 3, ω=5\omega = 5 (resonance), and ω=8\omega = 8.


Step 1 — Apply the formula at ω=3\omega = 3 (below resonance).

A(3)=1(259)2+(0.53)2A(3) = \dfrac{1}{\sqrt{(25 - 9)^{2} + (0.5 \cdot 3)^{2}}}

=1256+2.25= \dfrac{1}{\sqrt{256 + 2.25}}

=1258.25= \dfrac{1}{\sqrt{258.25}}

116.07\approx \dfrac{1}{16.07}

0.0622\approx 0.0622

A modest response — driving below resonance gives a small amplitude.

Step 2 — At ω=5\omega = 5 (resonance).

A(5)=1(2525)2+(0.55)2A(5) = \dfrac{1}{\sqrt{(25 - 25)^{2} + (0.5 \cdot 5)^{2}}}

=10+6.25= \dfrac{1}{\sqrt{0 + 6.25}}

=12.5= \dfrac{1}{2.5}

=0.4000= 0.4000

A massive response — about 6.4 times the off-resonance value at ω=3\omega = 3. The first term in the denominator vanishes, leaving only the damping term.

Step 3 — At ω=8\omega = 8 (above resonance).

A(8)=1(2564)2+(0.58)2A(8) = \dfrac{1}{\sqrt{(25 - 64)^{2} + (0.5 \cdot 8)^{2}}}

=11521+16= \dfrac{1}{\sqrt{1521 + 16}}

=11537= \dfrac{1}{\sqrt{1537}}

0.0255\approx 0.0255

Even smaller — driving above the natural frequency also gives a small response. The mass can't keep up with the rapid forcing.

Step 4 — The peak height.

At exact resonance, the amplitude is:

Apeak=F/mγω0=1(0.5)(5)=0.4A_{\text{peak}} = \dfrac{F/m}{\gamma\,\omega_0} = \dfrac{1}{(0.5)(5)} = 0.4

Smaller damping → larger peak. In the limit γ0\gamma \to 0 (no damping), the peak goes to infinity — the oscillator's amplitude grows without bound. This is what destroyed the Tacoma Narrows Bridge in 1940 (well, it was a more complex aeroelastic effect, but the principle is the same).

Step 5 — The "Q factor".

The sharpness of the resonance peak is measured by the quality factor:

Q=ω0γQ = \dfrac{\omega_0}{\gamma}

For our system: Q=5/0.5=10Q = 5/0.5 = 10. A pendulum clock might have Q100Q \sim 100, a quartz crystal Q106Q \sim 10^{6}, an atomic clock Q1014Q \sim 10^{14}. Higher Q = sharper resonance = more accurate timekeeping.


Answer:

  • A(3)0.062A(3) \approx 0.062 (off-resonance, small)
  • A(5)=0.400A(5) = 0.400resonance peak
  • A(8)0.026A(8) \approx 0.026 (above-resonance, small)

The amplitude peaks sharply at the natural frequency ω0=5\omega_0 = 5 — about 6× larger than even nearby frequencies. The peak height is 1/(γω0)1/(\gamma\omega_0), which goes to infinity as damping vanishes. The width of the peak is set by the quality factor Q=ω0/γQ = \omega_0/\gamma.

Try It

  • Slide the driving frequency through the natural frequency at 5 rad/s.
  • Watch the response amplitude grow dramatically near ω=ω0\omega = \omega_0.
  • Adjust the damping γ\gamma — smaller damping makes a sharper, taller peak.
  • The plot shows A(ω)A(\omega) across the entire frequency range.

Interactive Visualization

Parameters

5.00
0.50
Your turn

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Resonance: Peak Response at the Natural Frequency | MathSpin