
Physics III course sequence · Interactive lesson
Sound as displacement and pressure
Sound is one wave written in two variables. Learn to move between the displacement of the air and the pressure it creates, see why they sit a quarter cycle apart, and get the speed of sound from the stiffness and inertia of the medium rather than from a table.
UPIII-02.06 · Lesson 6 of 9 in this unit. Position is not a completion score.Build the model
The air moves one way; the pressure peaks a quarter wavelength away.
The key idea
A sound wave is a longitudinal displacement of the medium together with the pressure change it produces, that pressure being minus the bulk modulus times the displacement gradient, so the two run a quarter cycle out of step.
Example. A 1.00 kHz tone in air with pressure amplitude 0.0280 Pa displaces the air by only 1.08 × 10⁻⁸ m, because pₘₐₓ = ρ v ω sₘₐₓ and the factor ρ v ω is 2.59 × 10⁶ Pa per metre of displacement.
The complete physical model and assumptions
A sound wave in a fluid is one disturbance you can read in two languages. The primary variable is the longitudinal displacement s(x, t): each thin layer of air slides a little way along the direction of travel and back again. But a uniform slide compresses nothing, so what the ear and the microphone respond to is the gauge pressure, and that depends on how the displacement varies from layer to layer: p = −B ∂s/∂x, with B the bulk modulus. Differentiating a cosine gives a sine, so the two descriptions run a quarter cycle apart — the compressions sit where the air is momentarily back at its equilibrium position, not where it has moved furthest. Feed p = −B ∂s/∂x into Newton's second law for a slab of fluid and the linear wave equation appears with coefficient B/ρ, so v = √(B/ρ). In a gas the compressions are far too fast for heat to leak between them, so B is the adiabatic γP, not the isothermal P, and v = √(γRT/M): independent of pressure, independent of frequency, set by temperature and molar mass alone. The whole construction assumes the strain k sₘₐₓ stays far below 1, and it does: even in painfully loud sound, at a pressure amplitude of 200 Pa, the strain is only 1.4 × 10⁻³. But that small residual nonlinearity accumulates over distance, steepens the waveform, and eventually builds a shock the linear model cannot describe.
1The wave variable is a shift along the line of travel
On a string the displacement is transverse: y(x, t) points across the wave. A gas has no restoring force against a sideways shear, so the only mechanical wave it supports is longitudinal, and the wave variable is the displacement s(x, t) of a thin layer of air along the very axis the wave travels. Positive s means that layer has slid a little way toward +x; a moment later it slides back. Write it as s(x, t) = sₘₐₓ cos(kx − ωt), exactly the form used for a string, with k = 2π/λ, ω = 2πf and ω/k = v still holding. The scale is startling. A 1.00 kHz tone at ordinary conversational loudness has λ = 0.343 m in air but sₘₐₓ of order 10⁻⁸ m: the air shifts by about 3 × 10⁻⁸ of a wavelength. Sound is a very small disturbance riding on a very large background pressure, and that ratio is exactly what makes a linear treatment work.
2Only the gradient of the displacement compresses the gas
Take a slab of air between x and x + Δx with cross-section A, so its volume is A Δx. The face at x moves to x + s(x); the face at x + Δx moves to x + Δx + s(x + Δx). The new thickness is Δx + [s(x + Δx) − s(x)], so the fractional volume change is [s(x + Δx) − s(x)]/Δx, which becomes ∂s/∂x in the limit. Notice what that says: if every layer shifts by the same amount, ∂s/∂x = 0 and nothing is compressed — a wholesale translation of the air makes no sound at all. The bulk modulus is defined by B = −ΔP/(ΔV/V), the minus sign making B positive because squeezing raises the pressure. Substituting gives p(x, t) = −B ∂s/∂x, where p is the departure from ambient, not the absolute pressure. This is the partial derivative used operationally: hold t fixed, differentiate along x, and the result is a quantity a microphone can measure.
3A quarter cycle apart, and which one the ear reads
Differentiate: ∂s/∂x = −k sₘₐₓ sin(kx − ωt), so p(x, t) = B k sₘₐₓ sin(kx − ωt). A cosine has become a sine, which is a shift of a quarter cycle — a quarter period in time, a quarter wavelength in space. Where the displacement is at a crest the pressure is exactly ambient; where the displacement passes through zero the pressure is at a compression or a rarefaction. Now differentiate with respect to time instead: u = ∂s/∂t = ω sₘₐₓ sin(kx − ωt) is the air's own velocity, and it is in step with the pressure. Eliminating sₘₐₓ gives p = ρ v u, so pressure keeps company with velocity, not with displacement. It is the pressure the eardrum and the microphone diaphragm answer to. Comparing amplitudes, pₘₐₓ = B k sₘₐₓ = ρ v ω sₘₐₓ, and in air at 1.00 kHz that factor is 2.59 × 10⁶ Pa per metre. At the threshold of hearing, pₘₐₓ = 2.83 × 10⁻⁵ Pa, the air moves 1.09 × 10⁻¹¹ m — a tenth of an atomic diameter.
4Why v = √(B/ρ), and why B must be the adiabatic one
Apply Newton's second law to the same slab. The net force on it is A[p(x) − p(x + Δx)] = −A Δx ∂p/∂x, its mass is ρ A Δx, and its acceleration is ∂²s/∂t². Substituting p = −B ∂s/∂x gives B ∂²s/∂x² = ρ ∂²s/∂t², the linear wave equation with v² = B/ρ. Check the dimensions: [B]/[ρ] = (M L⁻¹ T⁻²)/(M L⁻³) = L² T⁻², a speed squared. Newton did this in 1687 and, assuming each compression stayed at ambient temperature, used B = P. That gives √(101325/1.204) = 290 m s⁻¹, some 15% below the measured value — a famous and honest failure. Laplace supplied the fix: an audio-frequency compression is far too quick for heat to leak out of it. In one period at 1.00 kHz heat diffuses only √(α/f) ≈ 0.15 mm in air, taking the thermal diffusivity α = 2.2 × 10⁻⁵ m² s⁻¹, against a wavelength of 343 mm, so each compression is thermally sealed. The right modulus is the adiabatic one, B = γP = 1.42 × 10⁵ Pa, and √(B/ρ) = 343 m s⁻¹.
5Temperature sets the speed in a gas; pressure does not
Substituting B = γP into v = √(B/ρ) gives v = √(γP/ρ), and the ideal-gas law written as ρ = PM/RT removes the pressure entirely: v = √(γRT/M). Raise the atmospheric pressure and the air stiffens and thickens in the same proportion, so the speed does not move. What is left is temperature and molar mass. Air at 0 °C gives √(1.40 × 8.314 × 273.15 / 0.02896) = 331 m s⁻¹, and at 20 °C, 343 m s⁻¹. Differentiating, dv/dT = v/2T = 0.59 m s⁻¹ per kelvin near room temperature, which is the familiar rule of about 0.6 m s⁻¹ per degree. Molar mass bites just as hard: helium, with γ = 5/3 and M = 4.00 g mol⁻¹, carries sound at 1.01 × 10³ m s⁻¹ at that same 20 °C. Note what is absent — the frequency. Within this model air is non-dispersive, which is why a chord played 30 m away still arrives as a chord.
6Where the small-amplitude model stops
Every step above assumed the strain |∂s/∂x| = k sₘₐₓ is small enough for B to count as constant. Put a number on it: a pressure amplitude of 200 Pa, loud enough to be painful, gives a strain of 200/141855 = 1.41 × 10⁻³, and a fractional pressure change of only 0.20%. Linearity looks safe, and locally it is. It still fails over distance. A compression is slightly hotter than ambient and is also carried forward on air that is itself moving, so a point on the waveform travels at v + βu with β = (γ + 1)/2 = 1.20 for air. Crests overtake the zero crossings, the waveform steepens, and after xₛ = ρv³/(βω pₘₐₓ) ≈ 32 m at 1.00 kHz the front goes vertical: a shock, whose own existence has destroyed the assumption that produced it. Two further limits sit outside the model — the continuum picture needs λ ≫ the 68 nm mean free path, and the lossless assumption ignores the viscous and thermal absorption that strips high frequencies over long ranges.
Key equations
Read the units, assumptions and limits before substituting.
Longitudinal displacement wave
s(x, t) = sₘₐₓ cos(kx − ωt + φ₀)
The wave variable is a shift of the air along x, not across it, so every result below is a derivative of this one.
s in m, measured along the direction of travel; k in rad m⁻¹, ω in rad s⁻¹Pressure from the displacement gradient
p(x, t) = −B ∂s/∂x
Only the gradient compresses the gas: shift every layer equally and no pressure appears at all.
p is gauge pressure in Pa, B the bulk modulus in Pa, and ∂s/∂x is dimensionlessPressure amplitude
pₘₐₓ = B k sₘₐₓ = ρ v ω sₘₐₓ
Converts between the two amplitudes, and shows why a high note is louder than a low one at the same displacement.
ρ in kg m⁻³, v in m s⁻¹, ω in rad s⁻¹; in air at 1.00 kHz, ρvω = 2.59 × 10⁶ Pa m⁻¹Pressure and particle velocity
p = ρ v u, where u = ∂s/∂t
For a wave going one way, pressure is in step with velocity even though it is a quarter cycle from displacement.
u is the air's own speed in m s⁻¹; ρv is the specific acoustic impedance in Pa s m⁻¹Wave speed from the medium
v = √(B/ρ)
Stiffness over inertia, the same shape as √(F/μ) on a string; nothing about the source enters.
B in Pa, ρ in kg m⁻³; water gives √(2.2 × 10⁹ ÷ 1000) = 1.48 × 10³ m s⁻¹Adiabatic ideal gas
v = √(γRT/M)
Follows from B = γP with ρ = PM/RT, so pressure cancels and only temperature and molar mass survive.
γ = CP/CV = 1.40 for air, R = 8.314 J mol⁻¹ K⁻¹, T in K, M in kg mol⁻¹Interactive lab
Predict first. Explore the model. Compare the result.
Explore the model
Try this. Push the frequency from 300 Hz to 800 Hz with the displacement amplitude held fixed: the wavelength shrinks and the pressure amplitude grows, reading {343/f|3} m and {1.2*343*2*π*f*sm/1000000|1} Pa at the current setting, then drag t and watch the quarter-wavelength offset stay locked.
Live results
- WAVELENGTH λ
- 0.686 m
- PRESSURE AMPLITUDE
- 15.52 Pa
- PARTICLE SPEED uₘₐₓ
- 0.038 m s⁻¹
- PEAK STRAIN ∂s/∂x
- 110 ×10⁻⁶
Results follow this lesson’s model and assumptions. Displayed values are rounded.
Predict → change one variable → check
Plan a change before running it. Every other input stays at the saved baseline.
Saved baseline. Displacement amplitude sₘₐₓ: 12 μm; Frequency f: 500 Hz; Time t: 0.00 ms
This experiment is kept only while this page is open. It does not change saved course progress.
Catch the common trap
The compressions are not where the air has moved furthest. Students reason that air pushed to the right must pile up where the push is largest, and so put the pressure maximum on the displacement maximum. But p = −B ∂s/∂x depends on the gradient, not on the value: shift every layer 10 nm to the right and nothing is compressed at all. At a displacement crest the neighbouring layers have moved almost exactly as far, the gradient vanishes, and the gauge pressure is zero — the air there is momentarily at rest and at ambient pressure. The compression sits a quarter wavelength away, where s passes through zero and the layers on either side are closing on each other. And the offset is a quarter cycle, not a half: the two curves are not inverted copies of one another, they are a sine and a cosine.
Practice & worked examples
3 authored examples. Make an attempt, then reveal the reasoning one step at a time.
EasyExample 1
A 1.00 kHz tone in air at 20 °C has pressure amplitude 0.0280 Pa. Taking ρ = 1.20 kg m⁻³ and v = 343 m s⁻¹, find the amplitude of the air's own velocity and the amplitude of its displacement, then compare that displacement with the wavelength.
Sketch your answer or reasoning, then compare it with the authored solution. Your writing is not automatically graded or saved.
0 of 4 steps revealed.
- For a wave travelling one way, pressure and particle velocity are in step and tied by p = ρ v u, so uₘₐₓ = pₘₐₓ/(ρv) = 0.0280 ÷ (1.20 × 343) = 0.0280/411.6 = 6.80 × 10⁻⁵ m s⁻¹.
- Displacement follows from u = ∂s/∂t: for s = sₘₐₓ cos(kx − ωt) the velocity amplitude is uₘₐₓ = ω sₘₐₓ, with ω = 2π × 1000 = 6.283 × 10³ rad s⁻¹.
- So sₘₐₓ = uₘₐₓ/ω = (6.80 × 10⁻⁵) ÷ 6283 = 1.08 × 10⁻⁸ m, about 11 nm.
- The wavelength is λ = v/f = 343/1000 = 0.343 m, so sₘₐₓ/λ = 3.2 × 10⁻⁸. Units check: pₘₐₓ/(ρvω) has Pa ÷ (kg m⁻³ × m s⁻¹ × s⁻¹) = (kg m⁻¹ s⁻²)/(kg m⁻² s⁻²) = m.
Answer. uₘₐₓ = 6.80 × 10⁻⁵ m s⁻¹ and sₘₐₓ = 1.08 × 10⁻⁸ m, roughly 3 × 10⁻⁸ of a wavelength. The air barely moves; it is the gradient of that motion the eardrum feels.
MediumExample 2
A 2.00 m tube is filled with argon at 20.0 °C and 101.3 kPa, and a sharp click takes 6.27 ms to cross it. Find the bulk modulus of the argon, deduce γ, and say what that value implies about the molecules. Argon has M = 39.95 g mol⁻¹.
Sketch your answer or reasoning, then compare it with the authored solution. Your writing is not automatically graded or saved.
0 of 5 steps revealed.
- Speed from the timing: v = L/t = 2.00 m ÷ (6.27 × 10⁻³ s) = 319 m s⁻¹.
- Density from the ideal-gas law: ρ = PM/RT = (101325 × 0.03995) ÷ (8.314 × 293.15) = 4048/2437 = 1.661 kg m⁻³.
- Invert v = √(B/ρ): B = ρv² = 1.661 × 319² = 1.661 × 1.018 × 10⁵ = 1.69 × 10⁵ Pa.
- Sound in a gas is adiabatic, so B = γP, giving γ = B/P = (1.69 × 10⁵) ÷ (1.013 × 10⁵) = 1.67.
- γ = 5/3 is the monatomic value: three translational degrees of freedom and no rotational or vibrational ones, exactly what a noble gas should show. Cross-check with √(γRT/M) = √(1.667 × 8.314 × 293.15 ÷ 0.03995) = 319 m s⁻¹.
Answer. B = 1.69 × 10⁵ Pa and γ = 1.67, that is 5/3 — the signature of a monatomic gas. Argon is slower than air despite the larger γ, because its molar mass is 1.38 times air's.
HardExample 3
A test siren radiates a 1.00 kHz tone of pressure amplitude 200 Pa into air at 20 °C, where ρ = 1.20 kg m⁻³, v = 343 m s⁻¹, P₀ = 101.3 kPa and γ = 1.40. First show the linear model is safe within one wavelength. Then, given that a point on the waveform really travels at v + βu with β = (γ + 1)/2, estimate the distance at which the wave steepens into a shock, using xₛ = ρv³/(βω pₘₐₓ).
Sketch your answer or reasoning, then compare it with the authored solution. Your writing is not automatically graded or saved.
0 of 5 steps revealed.
- Local strain: B = γP₀ = 1.40 × 101325 = 1.419 × 10⁵ Pa, so |∂s/∂x|ₘₐₓ = pₘₐₓ/B = 200/141855 = 1.41 × 10⁻³, while pₘₐₓ/P₀ = 200/101325 = 1.97 × 10⁻³. Both are far below 1, so across one wavelength the medium is linear to better than a fifth of a percent.
- Particle velocity: uₘₐₓ = pₘₐₓ/(ρv) = 200/411.6 = 0.486 m s⁻¹, an acoustic Mach number of 0.486/343 = 1.42 × 10⁻³. The displacement amplitude is uₘₐₓ/ω = 0.486/6283 = 7.73 × 10⁻⁵ m.
- Nonlinear coefficient: β = (γ + 1)/2 = (1.40 + 1)/2 = 1.20. A crest, riding on air already moving forward, outruns a zero crossing by βuₘₐₓ = 0.583 m s⁻¹ out of 343 m s⁻¹.
- Shock distance: xₛ = ρv³/(βω pₘₐₓ) = (1.20 × 4.035 × 10⁷) ÷ (1.20 × 6283 × 200) = (4.84 × 10⁷) ÷ (1.51 × 10⁶) = 32.1 m.
- Limiting check: xₛ ∝ 1/pₘₐₓ, so halving the amplitude doubles the distance, and as pₘₐₓ → 0 the shock distance runs to infinity. That is the correspondence the linear theory needs.
Answer. The strain is only 1.4 × 10⁻³, yet the wave steepens into a shock after about 32 m. Small-amplitude is a claim about one wavelength, not about a long path: a tiny error per cycle accumulates.
Quick check
Select an answer and explain it before checking.
Review & continue
A sound wave is a longitudinal displacement of the medium together with the pressure change it produces, that pressure being minus the bulk modulus times the displacement gradient, so the two run a quarter cycle out of step.
- Explain the relationship without looking at the equation.
- Check a sign, a unit and a model assumption in your working.
- Return to the lab or worked example if a step is still unclear.