Problem Set
NBPhO 2026
8. Jet Sound 8 pts
Decode a supersonic flyby spectrogram to extract the Mach number and closest-approach distance from the Doppler asymptotes and the sonic-boom delay.
Ingredients supersonic Doppler factorMach-cone geometrynon-monotonic emission-arrival maphead-on/tail-on asymptotes
medium
Prerequisites
- Doppler shift for a moving source,
- Speed of sound in still air; wavefronts as straight-line travelers
- Reading a logarithmic frequency axis
- Mach number and Mach angle,
Learning objectives
- Derive the supersonic Doppler factor and locate its zero at the Mach angle
- Recognise that for the source-time-to-observer-time map is non-monotonic, so each observer instant carries two arrivals
- Identify the sonic boom as the singular pile-up at and explain its broadband character
- Extract from the asymptote ratio and recover as the harmonic mean
- Convert the boom delay into a lateral distance via
Watch out for
- Treating the upper and lower curves as two different emitted tones. They are one emitted tone heard via two different propagation paths; the same governs both, and they meet at infinite frequency at the boom.
- Mis-anchoring the spectrogram's time origin. The boom delay is measured from the moment the jet flies overhead (visual sighting at ), not from the start of recording. The observer sees the jet several seconds before she hears it.
- Forgetting the absolute value in the Doppler factor. On the upstream branch (, jet still ahead) one has ; the observed frequency is , not a signed quantity.
- Reading a single descending Doppler curve as a subsonic flyby. A subsonic flyby produces one curve with a smooth high-to-low crossover. The presence of two simultaneous descending curves and a leading silence is the signature of .
- Confusing the Mach angle () with the look angle at which the boom arrives. The boom does pile up on the Mach cone, where , but refers to the cone's half-opening, while is the source-to-observer line of sight.