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Compressible Flow Simulator

Mach Angle & Mach Cone Calculator | Supersonic Geometry

Calculate Mach angle μ=arcsin(1/M), cone ground intersection and delay after overhead passage. Compare Mach 2 and 3 examples and distinguish the Mach angle from a finite shock angle.

Parameters
Mach number M
—
Sound speed c
m/s
Flight altitude h
m
Observer ground offset x
m
Presets
Playback speed
The orange source moves right and emits circular wavefronts at sound speed. Below M=1 they bunch ahead; at M=1 they form a wall; above M=1 their tangent envelope is the Mach cone. Use the presets to compare these regimes.
Observer x is a fixed ground position measured ahead of the source at restart. Restart repositions the source, observer and wavefronts. Changing M, sound speed or altitude also rebuilds the constant-condition history. The displayed delay is measured after overhead passage; arrival from restart is x/V plus that delay (M>1).
Results
—
Mach angle mu
—
Flight speed V
—
Boom arrival delay
—
Cone reach distance

—

Mach cone and ground boom

Orange source emits blue wavefront circles while moving right. Below M=1 the fronts bunch ahead; at M=1 they form a wall; above M=1 the yellow tangent lines form the Mach cone. Green: fixed observer; red cross: cone-ground crossing.

Mach-angle curve mu(M)

The curve is mu=arcsin(1/M), for M from1 to5. The marker shows the input only for M>=1; below1 the angle is undefined and no marker is drawn. Play advances wavefront time without changing M.

Theory & Key Formulas

Mach angle (cone half-angle):

$$\sin\mu = \frac{1}{M}, \qquad \mu = \arcsin\!\left(\frac{1}{M}\right)$$

Flight speed and ground reach distance of the cone:

$$V = M\,c, \qquad \ell = \frac{h}{\tan\mu}$$

Time delay of the boom (between the aircraft passing overhead and the cone reaching the observer below):

$$t_{\text{delay}} = \frac{\ell}{V} = \frac{h}{V\tan\mu} = \frac{h}{M\,c\,\tan\mu}$$

For $M\lt 1$ disturbances propagate ahead of the body and no cone forms; $M=1$ is a plane wave; only for $M\gt 1$ does the Mach cone appear. With the defaults $M=2,\ c=343\ \text{m/s},\ h=1000\ \text{m}$ this gives $\mu=30^\circ$, $V=686\ \text{m/s}$, $\ell=1732\ \text{m}$ and $t_{\text{delay}}=2.52\ \text{s}$.

Inputs and units

M is dimensionless; sound speed c is in m/s; altitude h and observer position x are in m. Here x is along the flight direction, not a lateral offset. Delay is measured after the source passes overhead.

Worked examples and checks

Mach 2 baseline

M=2, c=343 m/s, h=1000 m, x=0: V=686 m/s, μ=30.0°, ℓ≈1732 m and Δt≈2.52 s. The value 1000/343≈2.92 s is a vertical acoustic travel time, not this post-overhead delay.

Change to Mach 3

Keeping c and h fixed, M=3 gives V=1029 m/s, μ≈19.5°, ℓ≈2828 m and Δt≈2.75 s. The half-angle narrows while this delay increases. Doubling only altitude doubles both ℓ and Δt.

Equations and scope

A point source moves horizontally at constant V=Mc through a stationary, uniform medium. For M>1: μ=arcsin(1/M), ℓ=h/tanμ=h√(M²−1), Δt=ℓ/(Mc). ℓ is the horizontal distance behind the source to the ground intersection. This geometry does not calculate pressure amplitude, loudness, or refraction from wind and temperature layers.

Questions about the model

Is there a Mach cone at M≤1?

No cone forms for M<1. M=1 is the 90° half-angle limit, not a supersonic arrival-delay calculation.

Is the Mach angle the same as a shock angle?

Not generally. μ describes infinitesimal disturbances. The shock angle around a finite wedge or cone also depends on geometry and flow deflection.

Why does changing observer x leave Δt unchanged?

x is along the flight path. It changes the absolute overhead-passage time, but at constant altitude and speed the delay after that passage is unchanged.

References

NASA Glenn — Mach Angle

Read the theory

Explanation and examples checked: 9 September 2026

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🎬 Watch it in motion

Doppler Effect | break the sound barrier, get a shock cone #Shorts
Doppler Effect | break the sound barrier, get a shock cone #Shorts
Doppler Effect | break the sound barrier, get a shock cone #Shorts
Doppler Effect | break the sound barrier, get a shock cone #Shorts