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Speed of sound

From Wikipedia, the free encyclopedia
(Redirected fromSound velocity)
Speed of sound wave through elastic medium
For other uses, seeSpeed of sound (disambiguation).
AnF/A-18 Hornet displaying rare localized condensation at the speed of sound

Sound measurements
Characteristic
Symbols
 Sound pressure p, SPL,LPA
 Particle velocity v, SVL
 Particle displacement δ
 Sound intensity I, SIL
 Sound power P, SWL,LWA
 Sound energy W
 Sound energy density w
 Sound exposure E, SEL
 Acoustic impedance Z
 Audio frequency AF
 Transmission loss TL

Thespeed of sound is the distance travelled per unit of time by asound wave as it propagates through anelastic medium. More simply, the speed of sound is how fast vibrations travel. At 20 °C (68 °F), the speed of sound in air is about 343 m/s (1,125 ft/s; 1,235 km/h; 767 mph; 667 kn), orkm in2.92 s or onemile in4.69 s. It depends strongly on temperature as well as the medium through which asound wave is propagating.

At 0 °C (32 °F), the speed of sound in dryair (sea level 14.7 psi) is about 331 m/s (1,086 ft/s; 1,192 km/h; 740 mph; 643 kn).[1]

The speed of sound in anideal gas depends only on its temperature and composition. The speed has a weak dependence on frequency and pressure in dry air, deviating slightly from ideal behavior.

In colloquial speech,speed of sound refers to the speed of sound waves inair. However, the speed of sound varies from substance to substance: typically, sound travels most slowly ingases, faster inliquids, and fastest insolids.

For example, while sound travels at343 m/s in air, it travels at1481 m/s inwater (almost 4.3 times as fast) and at5120 m/s iniron (almost 15 times as fast). In an exceptionally stiff material such asdiamond, sound travels at 12,000 m/s (39,370 ft/s),[2] – about 35 times its speed in air and about the fastest it can travel under normal conditions.

In theory, the speed of sound is actually the speed of vibrations. Sound waves in solids are composed of compression waves (just as in gases and liquids) and a different type of sound wave called ashear wave, which occurs only in solids. Shear waves in solids usually travel at different speeds than compression waves, as exhibited inseismology. The speed of compression waves in solids is determined by the medium'scompressibility,shear modulus, and density. The speed of shear waves is determined only by the solid material's shear modulus and density.

Influid dynamics, the speed of sound in a fluid medium (gas or liquid) is used as a relative measure for the speed of an object moving through the medium. The ratio of the speed of an object to the speed of sound (in the same medium) is called the object'sMach number. Objects moving at speeds greater than the speed of sound (Mach1) are said to be traveling atsupersonic speeds.

Earth

[edit]

In Earth's atmosphere, the speed of sound varies greatly from about 295 m/s (1,060 km/h; 660 mph) at high altitudes to about 355 m/s (1,280 km/h; 790 mph) at high temperatures.

History

[edit]

Sir Isaac Newton's 1687Principia includes a computation of the speed of sound in air as 979 feet per second (298 m/s). This is too low by about 15%.[3] The discrepancy is due primarily to neglecting the (then unknown) effect of rapidly fluctuating temperature in a sound wave (in modern terms, sound wave compression and expansion of air is anadiabatic process, not anisothermal process). This error was later rectified byPierre-Simon Laplace.[4]

During the 17th century there were several attempts to measure the speed of sound accurately, including attempts byMarin Mersenne in 1630 (1,380 Parisian feet per second),Pierre Gassendi in 1635 (1,473 Parisian feet per second) andRobert Boyle (1,125 Parisian feet per second).[5] In 1709, the ReverendWilliam Derham,Rector of Upminster, published a more accurate measure of the speed of sound, at 1,072Parisian feet per second.[5] (TheParisian foot was325 mm. This is longer than the standard "international foot" in common use today, which was officially defined in 1959 as304.8 mm, making the speed of sound at 20 °C (68 °F) 1,055 Parisian feet per second).

Derham used a telescope from the tower of thechurch of St. Laurence, Upminster to observe the flash of a distant shotgun being fired, and then measured the time until he heard the gunshot with a half-second pendulum. Measurements were made of gunshots from a number of local landmarks, includingNorth Ockendon church. The distance was known bytriangulation, and thus the speed that the sound had travelled was calculated.[6]

Compression and shear waves

[edit]
Pressure-pulse or compression-type wave (longitudinal wave) confined to a plane. This is the only type of sound wave that travels in fluids (gases and liquids). A pressure-type wave may also travel in solids, along with other types of waves (transverse waves, see below).
Transverse wave affecting atoms initially confined to a plane. This additional type of sound wave (additional type of elastic wave) travels only in solids, for it requires a sideways shearing motion which is supported by the presence of elasticity in the solid. The sideways shearing motion may take place inany direction which is at right-angle to the direction of wave travel (only one shear direction is shown here, at right angles to the plane). Furthermore, the right-angle shear direction may change over time and distance, resulting in different types ofpolarization of shear waves.

In a gas or liquid, sound consists of compression waves. In solids, waves propagate as two different types. Alongitudinal wave is associated with compression and decompression in the direction of travel, and is the same process in gases and liquids, with an analogous compression-type wave in solids. Only compression waves are supported in gases and liquids. An additional type of wave, thetransverse wave, also called ashear wave, occurs only in solids because only solids support elastic deformations. It is due to elastic deformation of the medium perpendicular to the direction of wave travel; the direction of shear-deformation is called the "polarization" of this type of wave. In general, transverse waves occur as a pair oforthogonal polarizations.

These different waves (compression waves and the different polarizations of shear waves) may have different speeds at the same frequency. Therefore, they arrive at an observer at different times, an extreme example being anearthquake, where sharp compression waves arrive first and rocking transverse waves seconds later.

The speed of a compression wave in a fluid is determined by the medium'scompressibility anddensity. In solids, the compression waves are analogous to those in fluids, depending on compressibility and density, but with the additional factor ofshear modulus which affects compression waves due to off-axis elastic energies which are able to influence effective tension and relaxation in a compression. The speed of shear waves, which can occur only in solids, is determined simply by the solid material's shear modulus and density.

Equations

[edit]

The speed of sound in mathematical notation is conventionally represented byc, from the Latinceleritas meaning "swiftness".

For fluids in general, the speed of soundc is given by the Newton–Laplace equation:c=Ksρ,{\displaystyle c={\sqrt {\frac {K_{s}}{\rho }}},}where

Ks=ρ(Pρ)s{\displaystyle K_{s}=\rho \left({\frac {\partial P}{\partial \rho }}\right)_{s}}, whereP{\displaystyle P} is the pressure and thederivative is taken isentropically, that is, at constantentropys. This is because a sound wave travels so fast that its propagation can be approximated as anadiabatic process, meaning that there isn't enough time, during a pressure cycle of the sound, for significant heat conduction and radiation to occur.

Thus, the speed of sound increases with the stiffness (the resistance of an elastic body to deformation by an applied force) of the material and decreases with an increase in density. For ideal gases, the bulk modulusK is simply the gas pressure multiplied by the dimensionlessadiabatic index, which is about 1.4 for air under normal conditions of pressure and temperature.

For generalequations of state, ifclassical mechanics is used, the speed of soundc can be derived[7] as follows:

Consider the sound wave propagating at speedv{\displaystyle v} through a pipe aligned with thex{\displaystyle x} axis and with a cross-sectional area ofA{\displaystyle A}. In time intervaldt{\displaystyle dt} it moves lengthdx=vdt{\displaystyle dx=v\,dt}. Insteady state, themass flow ratem˙=ρvA{\displaystyle {\dot {m}}=\rho vA} must be the same at the two ends of the tube, therefore themass fluxj=ρv{\displaystyle j=\rho v} is constant andvdρ=ρdv{\displaystyle v\,d\rho =-\rho \,dv}. PerNewton's second law, thepressure-gradient force provides the acceleration:dvdt=1ρdPdxdP=(ρdv)dxdt=(vdρ)vv2c2=dPdρ{\displaystyle {\begin{aligned}{\frac {dv}{dt}}&=-{\frac {1}{\rho }}{\frac {dP}{dx}}\\[1ex]\rightarrow dP&=(-\rho \,dv){\frac {dx}{dt}}=(v\,d\rho )v\\[1ex]\rightarrow v^{2}&\equiv c^{2}={\frac {dP}{d\rho }}\end{aligned}}}

And therefore:

c=(Pρ)s=Ksρ,{\displaystyle c={\sqrt {\left({\frac {\partial P}{\partial \rho }}\right)_{s}}}={\sqrt {\frac {K_{s}}{\rho }}},}

Ifrelativistic effects are important, the speed of sound is calculated from therelativistic Euler equations.

In anon-dispersive medium, the speed of sound is independent ofsound frequency, so the speeds of energy transport and sound propagation are the same for all frequencies. Air, a mixture of oxygen and nitrogen, constitutes a non-dispersive medium. However, air does contain a small amount of CO2 whichis a dispersive medium, and causes dispersion to air atultrasonic frequencies (greater than28 kHz).[8]

In adispersive medium, the speed of sound is a function of sound frequency, through thedispersion relation. Each frequency component propagates at its own speed, called thephase velocity, while the energy of the disturbance propagates at thegroup velocity. The same phenomenon occurs with light waves; seeoptical dispersion for a description.

Dependence on the properties of the medium

[edit]

The speed of sound is variable and depends on the properties of the substance through which the wave is travelling. In solids, the speed of transverse (or shear) waves depends on the shear deformation undershear stress (called theshear modulus), and the density of the medium. Longitudinal (or compression) waves in solids depend on the same two factors with the addition of a dependence oncompressibility.

In fluids, only the medium's compressibility and density are the important factors, since fluids do not transmit shear stresses. In heterogeneous fluids, such as a liquid filled with gas bubbles, the density of the liquid and the compressibility of the gas affect the speed of sound in an additive manner, as demonstrated in thehot chocolate effect.

In gases, adiabatic compressibility is directly related to pressure through theheat capacity ratio (adiabatic index), while pressure and density are inversely related to the temperature and molecular weight, thus making only the completely independent properties oftemperature and molecular structure important (heat capacity ratio may be determined by temperature and molecular structure, but simple molecular weight is not sufficient to determine it).

Sound propagates faster in lowmolecular weight gases such ashelium than it does in heavier gases such asxenon. For monatomic gases, the speed of sound is about 75% of the mean speed that the atoms move in that gas.

For a givenideal gas the molecular composition is fixed, and thus the speed of sound depends only on itstemperature. At a constant temperature, the gaspressure has no effect on the speed of sound, since the density will increase, and since pressure anddensity (also proportional to pressure) have equal but opposite effects on the speed of sound, and the two contributions cancel out exactly. In a similar way, compression waves in solids depend both on compressibility and density—just as in liquids—but in gases the density contributes to the compressibility in such a way that some part of each attribute factors out, leaving only a dependence on temperature, molecular weight, and heat capacity ratio which can be independently derived from temperature and molecular composition (see derivations below). Thus, for a single given gas (assuming the molecular weight does not change) and over a small temperature range (for which the heat capacity is relatively constant), the speed of sound becomes dependent on only the temperature of the gas.

In non-ideal gas behavior regimen, for which theVan der Waals gas equation would be used, the proportionality is not exact, and there is a slight dependence of sound velocity on the gas pressure.

Humidity has a small but measurable effect on the speed of sound (causing it to increase by about 0.1%–0.6%), becauseoxygen andnitrogen molecules of the air are replaced by lighter molecules ofwater. This is a simple mixing effect.

Altitude variation and implications for atmospheric acoustics

[edit]
Density and pressure decrease smoothly with altitude, but temperature (red) does not. The speed of sound (blue) depends only on the complicated temperature variation at altitude and can be calculated from it since isolated density and pressure effects on the speed of sound cancel each other. The speed of sound increases with height in two regions of the stratosphere and thermosphere, due to heating effects in these regions.

In theEarth's atmosphere, the chief factor affecting the speed of sound is thetemperature. For a given ideal gas with constant heat capacity and composition, the speed of sound is dependentsolely upon temperature; see§ Details below. In such an ideal case, the effects of decreased density and decreased pressure of altitude cancel each other out, save for the residual effect of temperature.

Since temperature (and thus the speed of sound) decreases with increasing altitude up to11 km, sound isrefracted upward, away from listeners on the ground, creating anacoustic shadow at some distance from the source.[9] The decrease of the speed of sound with height is referred to as a negativesound speed gradient.

However, there are variations in this trend above11 km. In particular, in thestratosphere above about20 km, the speed of sound increases with height, due to an increase in temperature from heating within theozone layer. This produces a positive speed of sound gradient in this region. Still another region of positive gradient occurs at very high altitudes, in thethermosphere above90 km.

Details

[edit]

Speed of sound in ideal gases and air

[edit]

For an ideal gas,K (thebulk modulus in equations above, equivalent toC, the coefficient of stiffness in solids) is given byK=γp.{\displaystyle K=\gamma \cdot p.}Thus, from the Newton–Laplace equation above, the speed of sound in an ideal gas is given byc=γpρ,{\displaystyle c={\sqrt {\gamma \cdot {p \over \rho }}},}where

  • γ is theadiabatic index also known as theisentropic expansion factor. It is the ratio of the specific heat of a gas at constant pressure to that of a gas at constant volume (Cp/Cv{\displaystyle C_{p}/C_{v}}) and arises because a classical sound wave induces an adiabatic compression, in which the heat of the compression does not have enough time to escape the pressure pulse, and thus contributes to the pressure induced by the compression;
  • p is thepressure;
  • ρ is thedensity.

Using theideal gas law to replacep withnRT/V, and replacingρ withnM/V, the equation for an ideal gas becomescideal=γpρ=γRTM=γkTm,{\displaystyle c_{\mathrm {ideal} }={\sqrt {\gamma \cdot {p \over \rho }}}={\sqrt {\gamma \cdot R\cdot T \over M}}={\sqrt {\gamma \cdot k\cdot T \over m}},}where

  • cideal is the speed of sound in anideal gas;
  • R is the specificmolar gas constant;
  • k is theBoltzmann constant;
  • γ (gamma) is theadiabatic index. At room temperature, where thermal energy is fully partitioned into rotation (rotations are fully excited) but quantum effects prevent excitation of vibrational modes, the value is7/5 = 1.400 for diatomic gases (such asoxygen andnitrogen), according to kinetic theory. Gamma is actually experimentally measured over a range from 1.3991 to 1.403 at0 °C, for air. Gamma is exactly5/3 = 1.667 for monatomic gases (such asargon) and it is4/3 = 1.333 for triatomic molecule gases that, likeH
    2
    O
    , are not co-linear (a co-linear triatomic gas such asCO
    2
    is equivalent to a diatomic gas for our purposes here);
  • T is the absolute temperature;
  • M is the molar mass of the gas. The mean molar mass for dry air is about 0.02897 kg/mol (28.97 g/mol);
  • n is the number of moles;
  • m is the mass of a single molecule.

This equation applies only when the sound wave is a small perturbation on the ambient condition, and the certain other noted conditions are fulfilled, as noted below. Calculated values forcair have been found to vary slightly from experimentally determined values.[10]

Newton famously considered the speed of sound before most of the development ofthermodynamics and so incorrectly usedisothermal calculations instead ofadiabatic. His result was missing the factor ofγ but was otherwise correct.

Numerical substitution of the above values gives the ideal gas approximation of sound velocity for gases, which is accurate at relatively low gas pressures and densities (for air, this includes standard Earth sea-level conditions). Also, for diatomic gases the use ofγ = 1.4000 requires that the gas exists in a temperature range high enough that rotational heat capacity is fully excited (i.e., molecular rotation is fully used as a heat energy "partition" or reservoir); but at the same time the temperature must be low enough that molecular vibrational modes contribute no heat capacity (i.e., insignificant heat goes into vibration, as all vibrational quantum modes above the minimum-energy-mode have energies that are too high to be populated by a significant number of molecules at this temperature). For air, these conditions are fulfilled at room temperature, and also temperatures considerably below room temperature (see tables below). See the section on gases inspecific heat capacity for a more complete discussion of this phenomenon.

For air, we introduce the shorthandR=R/Mair.{\displaystyle R_{*}=R/M_{\mathrm {air} }.}

Approximation of the speed of sound in dry air based on theheat capacity ratio (in green) against the truncatedTaylor expansion (in red)

In addition, we switch to theCelsius temperatureθ =T273.15 K, which is useful to calculate air speed in the region near0 °C (273 K). Then, for dry air,cair=γRT=γR(θ+273.15K),cair=γR273.15K1+θ273.15K.{\displaystyle {\begin{aligned}c_{\mathrm {air} }&={\sqrt {\gamma \cdot R_{*}\cdot T}}={\sqrt {\gamma \cdot R_{*}\cdot (\theta +273.15\,\mathrm {K} )}},\\c_{\mathrm {air} }&={\sqrt {\gamma \cdot R_{*}\cdot 273.15\,\mathrm {K} }}\cdot {\sqrt {1+{\frac {\theta }{273.15\,\mathrm {K} }}}}.\end{aligned}}}

Substituting numerical valuesR=8.31446261815324 J/(molK){\displaystyle R=8.314\,462\,618\,153\,24~\mathrm {J/(mol{\cdot }K)} }Mair=0.0289645 kg/mol{\displaystyle M_{\mathrm {air} }=0.028\,964\,5~\mathrm {kg/mol} }and using the ideal diatomic gas value ofγ = 1.4000, we havecair331.3m/s×1+θ273.15K.{\displaystyle c_{\mathrm {air} }\approx 331.3\,\mathrm {m/s} \times {\sqrt {1+{\frac {\theta }{273.15\,\mathrm {K} }}}}.}

Finally, Taylor expansion of the remaining square root inθ{\displaystyle \theta } yieldscair331.3m/s×(1+θ2×273.15K),331.3m/s+θ×0.606(m/s)/C.{\displaystyle {\begin{aligned}c_{\mathrm {air} }&\approx 331.3\,\mathrm {m/s} \times \left(1+{\frac {\theta }{2\times 273.15\,\mathrm {K} }}\right),\\&\approx 331.3\,\mathrm {m/s} +\theta \times 0.606\,\mathrm {(m/s)/^{\circ }C} .\end{aligned}}}

A graph comparing results of the two equations is to the right, using the slightly more accurate value of 331.5 m/s (1,088 ft/s) for the speed of sound at0 °C.[11]: 120-121 

Effects due to wind shear

[edit]

The speed of sound varies with temperature. Since temperature and sound velocity normally decrease with increasing altitude, sound isrefracted upward, away from listeners on the ground, creating anacoustic shadow at some distance from the source.[9] Wind shear of 4 m/(s · km) can produce refraction equal to a typical temperaturelapse rate of7.5 °C/km.[12] Higher values of wind gradient will refract sound downward toward the surface in the downwind direction,[13] eliminating the acoustic shadow on the downwind side. This will increase the audibility of sounds downwind. This downwind refraction effect occurs because there is a wind gradient; the fact that sound is carried along by the wind is not important.[14]

For sound propagation, the exponential variation of wind speed with height can be defined as follows:[15]U(h)=U(0)hζ,dUdH(h)=ζU(h)h,{\displaystyle {\begin{aligned}U(h)&=U(0)h^{\zeta },\\{\frac {\mathrm {d} U}{\mathrm {d} H}}(h)&=\zeta {\frac {U(h)}{h}},\end{aligned}}}where

  • U(h) is the speed of the wind at heighth;
  • ζ is the exponential coefficient based on ground surface roughness, typically between 0.08 and 0.52;
  • dU/dH(h) is the expected wind gradient at heighth.

In the 1862American Civil WarBattle of Iuka, an acoustic shadow, believed to have been enhanced by a northeast wind, kept two divisions of Union soldiers out of the battle,[16] because they could not hear the sounds of battle only10 km (six miles) downwind.[17]

Tables

[edit]

In thestandard atmosphere:

  • T0 is273.15 K (=0 °C =32 °F), giving a theoretical value of331.3 m/s (=1086.9 ft/s =1193 km/h =741.1 mph =644.0kn). Values ranging from 331.3 to331.6 m/s may be found in reference literature, however;
  • T20 is293.15 K (=20 °C =68 °F), giving a value of343.2 m/s (=1126.0 ft/s =1236 km/h =767.8 mph =667.2kn);
  • T25 is298.15 K (=25 °C =77 °F), giving a value of346.1 m/s (=1135.6 ft/s =1246 km/h =774.3 mph =672.8kn).

In fact, assuming anideal gas, the speed of soundc depends on temperature and composition only,not on the pressure ordensity (since these change in lockstep for a given temperature and cancel out). Air is almost an ideal gas. The temperature of the air varies with altitude, giving the following variations in the speed of sound using the standard atmosphere—actual conditions may vary.[citation needed]

Effect of temperature on properties of air
Celsius
tempe­rature
θ [°C]
Speed of
sound
c [m/s]
Density
of air
ρ [kg/m3]
Characteristic specific
acoustic impedance
z0 [Pas/m]
35351.881.1455403.2
30349.021.1644406.5
25346.131.1839409.4
20343.211.2041413.3
15340.271.2250416.9
10337.311.2466420.5
5334.321.2690424.3
0331.301.2922428.0
−5328.251.3163432.1
−10325.181.3413436.1
−15322.071.3673440.3
−20318.941.3943444.6
−25315.771.4224449.1

Given normal atmospheric conditions, the temperature, and thus speed of sound, varies with altitude:

AltitudeTemperaturem/skm/hmphkn
Sea level15 °C (59 °F)3401,225761661
11,000 m to20,000 m
(cruising altitude of commercial jets,
andfirst supersonic flight)
−57 °C (−70 °F)2951,062660573
29,000 m (flight ofX-43A)−48 °C (−53 °F)3011,083673585

Effect of frequency and gas composition

[edit]

General physical considerations

[edit]

The medium in which a sound wave is travelling does not always respond adiabatically, and as a result, the speed of sound can vary with frequency.[18]

The limitations of the concept of speed of sound due to extreme attenuation are also of concern. The attenuation which exists at sea level for high frequencies applies to successively lower frequencies as atmospheric pressure decreases, or as themean free path increases. For this reason, the concept of speed of sound (except for frequencies approaching zero) progressively loses its range of applicability at high altitudes.[10] The standard equations for the speed of sound apply with reasonable accuracy only to situations in which the wavelength of the sound wave is considerably longer than the mean free path of molecules in a gas.

The molecular composition of the gas contributes both as the mass (M) of the molecules, and their heat capacities, and so both have an influence on speed of sound. In general, at the same molecular mass, monatomic gases have slightly higher speed of sound (over 9% higher) because they have a higherγ (5/3 = 1.66...) than diatomics do (7/5 = 1.4). Thus, at the same molecular mass, the speed of sound of a monatomic gas goes up by a factor ofcgas,monatomiccgas,diatomic=5/37/5=2521=1.091{\displaystyle {c_{\mathrm {gas,monatomic} } \over c_{\mathrm {gas,diatomic} }}={\sqrt {{5/3} \over {7/5}}}={\sqrt {25 \over 21}}=1.091\ldots }

This gives the 9% difference, and would be a typical ratio for speeds of sound at room temperature inhelium vs.deuterium, each with a molecular weight of 4. Sound travels faster in helium than deuterium because adiabatic compression heats helium more since the helium molecules can store heat energy from compression only in translation, but not rotation. Thus helium molecules (monatomic molecules) travel faster in a sound wave and transmit sound faster. (Sound travels at about 70% of the mean molecular speed in gases; the figure is 75% in monatomic gases and 68% in diatomic gases).

In this example we have assumed that temperature is low enough that heat capacities are not influenced by molecular vibration (seeheat capacity). However, vibrational modes simply cause gammas which decrease toward 1, since vibration modes in a polyatomic gas give the gas additional ways to store heat which do not affect temperature, and thus do not affect molecular velocity and sound velocity. Thus, the effect of higher temperatures and vibrational heat capacity acts to increase the difference between the speed of sound in monatomic vs. polyatomic molecules, with the speed remaining greater in monatomics.

Practical application to air

[edit]

By far, the most important factor influencing the speed of sound in air is temperature. The speed is proportional to the square root of the absolute temperature, giving an increase of about0.6 m/s per degree Celsius. For this reason, the pitch of a musical wind instrument increases as its temperature increases.

The speed of sound is raised by humidity. The difference between 0% and 100% humidity is about1.5 m/s at standard pressure and temperature, but the size of the humidity effect increases dramatically with temperature.

The dependence on frequency and pressure are normally insignificant in practical applications. In dry air, the speed of sound increases by about0.1 m/s as the frequency rises from10 Hz to100 Hz. For audible frequencies above100 Hz it is relatively constant. Standard values of the speed of sound are quoted in the limit of low frequencies, where the wavelength is large compared to the mean free path.[19]

As shown above, the approximate value 1000/3 = 333.33... m/s is exact a little below5 °C and is a good approximation for all "usual" outside temperatures (in temperate climates, at least), hence the usual rule of thumb to determine how far lightning has struck: count the seconds from the start of the lightning flash to the start of the corresponding roll of thunder and divide by 3: the result is the distance in kilometers to the nearest point of the lightning bolt. Or divide the number of seconds by 5 for an approximate distance in miles.

Mach number

[edit]
Main article:Mach number

Mach number, a useful quantity in aerodynamics, is the ratio of airspeed to the local speed of sound. At altitude, for reasons explained, Mach number is a function of temperature.Aircraftflight instruments, however, operate using pressure differential to compute Mach number, not temperature. The assumption is that a particular pressure represents a particular altitude and, therefore, a standard temperature. Aircraft flight instruments need to operate this way because the stagnation pressure sensed by aPitot tube is dependent on altitude as well as speed.

Experimental methods

[edit]

A range of different methods exist for the measurement of the speed of sound in air.

The earliest reasonably accurate estimate of the speed of sound in air was made byWilliam Derham and acknowledged byIsaac Newton. Derham had a telescope at the top of the tower of theChurch of St Laurence inUpminster, England. On a calm day, a synchronized pocket watch would be given to an assistant who would fire a shotgun at a pre-determined time from a conspicuous point some miles away, across the countryside. This could be confirmed by telescope. He then measured the interval between seeing gunsmoke and arrival of the sound using a half-second pendulum. The distance from where the gun was fired was found by triangulation, and simple division (distance/time) provided velocity. Lastly, by making many observations, using a range of different distances, the inaccuracy of the half-second pendulum could be averaged out, giving his final estimate of the speed of sound. Modern stopwatches enable this method to be used today over distances as short as 200–400 metres, and not needing something as loud as a shotgun.

Single-shot timing methods

[edit]

The simplest concept is the measurement made using twomicrophones and a fast recording device such as adigital storage scope. This method uses the following idea.

If a sound source and two microphones are arranged in a straight line, with the sound source at one end, then the following can be measured:

  1. The distance between the microphones (x), called microphone basis.
  2. The time of arrival between the signals (delay) reaching the different microphones (t).

Thenv =x/t.

Other methods

[edit]

In these methods, thetime measurement has been replaced by a measurement of the inverse of time (frequency).

Kundt's tube is an example of an experiment which can be used to measure the speed of sound in a small volume. It has the advantage of being able to measure the speed of sound in any gas. This method uses a powder to make thenodes andantinodes visible to the human eye. This is an example of a compact experimental setup.

Atuning fork can be held near the mouth of a longpipe which is dipping into a barrel ofwater. In this system it is the case that the pipe can be brought to resonance if the length of the air column in the pipe is equal to(1 + 2n)λ/4 wheren is an integer. As theantinodal point for the pipe at the open end is slightly outside the mouth of the pipe it is best to find two or more points of resonance and then measure half a wavelength between these.

Here it is the case thatv =.

High-precision measurements in air

[edit]

The effect of impurities can be significant when making high-precision measurements. Chemicaldesiccants can be used to dry the air, but will, in turn, contaminate the sample. The air can be dried cryogenically, but this has the effect of removing the carbon dioxide as well; therefore many high-precision measurements are performed with air free of carbon dioxide rather than with natural air. A 2002 review[20] found that a 1963 measurement by Smith and Harlow using a cylindrical resonator gave "the most probable value of the standard speed of sound to date." The experiment was done with air from which the carbon dioxide had been removed, but the result was then corrected for this effect so as to be applicable to real air. The experiments were done at30 °C but corrected for temperature in order to report them at0 °C. The result was331.45 ± 0.01 m/s for dry air at STP, for frequencies from93 Hz to1,500 Hz.

Non-gaseous media

[edit]

Speed of sound in solids

[edit]

Three-dimensional solids

[edit]

In a solid, there is a non-zero stiffness both for volumetric deformations and shear deformations. Hence, it is possible to generate sound waves with different velocities dependenton the deformation mode. Sound waves generating volumetric deformations (compression) and shear deformations (shearing) are called pressure waves (longitudinal waves) and shear waves (transverse waves), respectively. Inearthquakes, the corresponding seismic waves are calledP-waves (primary waves) andS-waves (secondary waves), respectively. The sound velocities of these two types of waves propagating in a homogeneous 3-dimensional solid are respectively given by[11]csolid,p=K+43Gρ=E(1ν)ρ(1+ν)(12ν),{\displaystyle c_{\mathrm {solid,p} }={\sqrt {\frac {K+{\frac {4}{3}}G}{\rho }}}={\sqrt {\frac {E(1-\nu )}{\rho (1+\nu )(1-2\nu )}}},}csolid,s=Gρ,{\displaystyle c_{\mathrm {solid,s} }={\sqrt {\frac {G}{\rho }}},}where

The last quantity is not an independent one, asE = 3K(1 − 2ν). The speed of pressure waves depends both on the pressure and shear resistance properties of the material, while the speed of shear waves depends on the shear properties only.

Typically, pressure waves travel faster in materials than do shear waves, and in earthquakes this is the reason that the onset of an earthquake is often preceded by a quick upward-downward shock, before arrival of waves that produce a side-to-side motion. For example, for a typical steel alloy,K = 170 GPa,G = 80 GPa andp =7700 kg/m3, yielding a compressional speedcsolid,p of6,000 m/s.[11] This is in reasonable agreement withcsolid,p measured experimentally at5,930 m/s for a (possibly different) type of steel.[21] The shear speedcsolid,s is estimated at3,200 m/s using the same numbers.

Speed of sound in semiconductor solids can be very sensitive to the amount of electronic dopant in them.[22]

One-dimensional solids

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The speed of sound for pressure waves in stiff materials such as metals is sometimes given for "long rods" of the material in question, in which the speed is easier to measure. In rods where their diameter is shorter than a wavelength, the speed of pure pressure waves may be simplified and is given by:[11]: 70csolid=Eρ,{\displaystyle c_{\mathrm {solid} }={\sqrt {\frac {E}{\rho }}},}whereE isYoung's modulus. This is similar to the expression for shear waves, save thatYoung's modulus replaces theshear modulus. This speed of sound for pressure waves in long rods will always be slightly less than the same speed in homogeneous 3-dimensional solids, and the ratio of the speeds in the two different types of objects depends onPoisson's ratio for the material.

Speed of sound in liquids

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Speed of sound in water vs temperature

In a fluid, the only non-zerostiffness is to volumetric deformation (a fluid does not sustain shear forces).

Hence the speed of sound in a fluid is given bycfluid=Kρ,{\displaystyle c_{\mathrm {fluid} }={\sqrt {\frac {K}{\rho }}},}whereK is thebulk modulus of the fluid.

Water

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In fresh water, sound travels at about1481 m/s at20 °C (see the External Links section below for online calculators).[23] Applications ofunderwater sound can be found insonar,acoustic communication andacoustical oceanography.

Seawater

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See also:Sound speed profile
Speed of sound as a function of depth at a position north of Hawaii in thePacific Ocean derived from the 2005World Ocean Atlas. TheSOFAR channel spans the minimum in the speed of sound at about 750 m depth.

In salt water that is free of air bubbles or suspended sediment, sound travels at about1500 m/s (1500.235 m/s at1000 kilopascals,10 °C and 3%salinity by one method).[24] The speed of sound in seawater depends on pressure (hence depth), temperature (a change of1 °C ~4 m/s), andsalinity (a change of 1 ~1 m/s), and empirical equations have been derived to accurately calculate the speed of sound from these variables.[25][26] Other factors affecting the speed of sound are minor. Since in most ocean regions temperature decreases with depth, the profile of the speed of sound with depth decreases to a minimum at a depth of several hundred metres. Below the minimum, sound speed increases again, as the effect of increasing pressure overcomes the effect of decreasing temperature (right).[27] For more information see Dushaw et al.[28]

An empirical equation for the speed of sound in sea water is provided by Mackenzie:[29]c(T,S,z)=a1+a2T+a3T2+a4T3+a5(S35)+a6z+a7z2+a8T(S35)+a9Tz3,{\displaystyle c(T,S,z)=a_{1}+a_{2}T+a_{3}T^{2}+a_{4}T^{3}+a_{5}(S-35)+a_{6}z+a_{7}z^{2}+a_{8}T(S-35)+a_{9}Tz^{3},}where

  • T is the temperature in degrees Celsius;
  • S is the salinity in parts per thousand;
  • z is the depth in metres.

The constantsa1,a2, ...,a9 area1=1,448.96,a2=4.591,a3=5.304×102,a4=2.374×104,a5=1.340,a6=1.630×102,a7=1.675×107,a8=1.025×102,a9=7.139×1013,{\displaystyle {\begin{aligned}a_{1}&=1,448.96,&a_{2}&=4.591,&a_{3}&=-5.304\times 10^{-2},\\a_{4}&=2.374\times 10^{-4},&a_{5}&=1.340,&a_{6}&=1.630\times 10^{-2},\\a_{7}&=1.675\times 10^{-7},&a_{8}&=-1.025\times 10^{-2},&a_{9}&=-7.139\times 10^{-13},\end{aligned}}}with check value1550.744 m/s forT =25 °C,S = 35 parts per thousand,z = 1,000 m. This equation has a standard error of0.070 m/s for salinity between 25 and 40ppt. See[1] for an online calculator.

(The Sound Speed vs. Depth graph doesnot correlate directly to the MacKenzie formula.This is due to the fact that the temperature and salinity varies at different depths.WhenT andS are held constant, the formula itself is always increasing with depth.)

Other equations for the speed of sound in sea water are accurate over a wide range of conditions, but are far more complicated, e.g., that by V. A. Del Grosso[30] and the Chen-Millero-Li Equation.[28][31]

Speed of sound in plasma

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The speed of sound in aplasma for the common case that the electrons are hotter than the ions (but not too much hotter) is given by the formula (seehere)cs=(γZkTemi)1/2=(γZTeμ)1/2×90.85 m/s,{\displaystyle c_{s}=\left({\frac {\gamma ZkT_{\mathrm {e} }}{m_{\mathrm {i} }}}\right)^{1/2}=\left({\frac {\gamma ZT_{e}}{\mu }}\right)^{1/2}\times 90.85~\mathrm {m/s} ,}where

In contrast to a gas, the pressure and the density are provided by separate species: the pressure by the electrons and the density by the ions. The two are coupled through a fluctuating electric field.

Mars

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The speed of sound onMars varies as a function of frequency. Higher frequencies travel faster than lower frequencies. Higher frequency sound from lasers travels at 250 m/s (820 ft/s), while low frequency sound travels at 240 m/s (790 ft/s).[32]

Gradients

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Main article:Sound speed gradient

When sound spreads out evenly in all directions in three dimensions, the intensity drops in proportion to the inverse square of the distance. However, in the ocean, there is a layer called the 'deep sound channel' orSOFAR channel which can confine sound waves at a particular depth.

In the SOFAR channel, the speed of sound is lower than that in the layers above and below. Just as light waves will refract towards a region of higherrefractive index, sound waves willrefract towards a region where their speed is reduced. The result is that sound gets confined in the layer, much the way light can be confined to a sheet of glass oroptical fiber. Thus, the sound is confined in essentially two dimensions. In two dimensions the intensity drops in proportion to only the inverse of the distance. This allows waves to travel much further before being undetectably faint.

A similar effect occurs in the atmosphere.Project Mogul successfully used this effect to detect anuclear explosion at a considerable distance.

See also

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References

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  1. ^"Speed of Sound Calculator".National Weather Service. Retrieved23 July 2021.
  2. ^C. R. Nave."Speed of Sound".HyperPhysics. Department of Physics and Astronomy, Georgia State University. Retrieved24 October 2022.
  3. ^"The Speed of Sound". mathpages.com. Retrieved3 May 2015.
  4. ^Bannon, Mike; Kaputa, Frank (12 December 2014)."The Newton–Laplace Equation and Speed of Sound". Thermal Jackets. Retrieved3 May 2015.
  5. ^abMurdin, Paul (25 December 2008).Full Meridian of Glory: Perilous Adventures in the Competition to Measure the Earth. Springer Science & Business Media. pp. 35–36.ISBN 9780387755342.
  6. ^Fox, Tony (2003).Essex Journal. Essex Arch & Hist Soc. pp. 12–16.
  7. ^"17.2 Speed of Sound | University Physics Volume 1".courses.lumenlearning.com. Retrieved24 January 2020.
  8. ^Dean, E. A. (August 1979).Atmospheric Effects on the Speed of Sound, Technical report of Defense Technical Information Center
  9. ^abEverest, F. (2001).The Master Handbook of Acoustics. New York: McGraw-Hill. pp. 262–263.ISBN 978-0-07-136097-5.
  10. ^abU.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976.
  11. ^abcdKinsler, L.E.; Frey, A.R.; Coppens, A.B.; Sanders, J.V. (2000).Fundamentals of Acoustics (4th ed.). New York: John Wiley & Sons.ISBN 0-471-84789-5.
  12. ^Uman, Martin (1984).Lightning. New York: Dover Publications.ISBN 978-0-486-64575-9.
  13. ^Volland, Hans (1995).Handbook of Atmospheric Electrodynamics. Boca Raton: CRC Press. p. 22.ISBN 978-0-8493-8647-3.
  14. ^Singal, S. (2005).Noise Pollution and Control Strategy. Oxford: Alpha Science International. p. 7.ISBN 978-1-84265-237-4.It may be seen that refraction effects occur only because there is a wind gradient and it is not due to the result of sound being convected along by the wind.
  15. ^Bies, David (2009).Engineering Noise Control, Theory and Practice. London: CRC Press. p. 249.ISBN 978-0-415-26713-7.As wind speed generally increases with altitude, wind blowing towards the listener from the source will refract sound waves downwards, resulting in increased noise levels.
  16. ^Cornwall, Sir (1996).Grant as Military Commander. New York: Barnes & Noble. p. 92.ISBN 978-1-56619-913-1.
  17. ^Cozens, Peter (2006).The Darkest Days of the War: the Battles of Iuka and Corinth. Chapel Hill: The University of North Carolina Press.ISBN 978-0-8078-5783-0.
  18. ^A B Wood, A Textbook of Sound (Bell, London, 1946)
  19. ^"Speed of Sound in Air". Phy.mtu.edu. Retrieved13 June 2014.
  20. ^Zuckerwar, Handbook of the speed of sound in real gases, p. 52
  21. ^J. Krautkrämer and H. Krautkrämer (1990),Ultrasonic testing of materials, 4th fully revised edition, Springer-Verlag, Berlin, Germany, p. 497
  22. ^Slade, Tyler; Anand, Shashwat; Wood, Max; Male, James; Imasato, Kazuki; Cheikh, Dean; Al Malki, Muath; Agne, Matthias; Griffith, Kent; Bux, Sabah; Wolverton, Chris; Kanatzidis, Mercouri; Snyder, Jeff (2021)."Charge-carrier-mediated lattice softening contributes to high zT in thermoelectric semiconductors".Joule.5 (5): 1168-1182.Bibcode:2021Joule...5.1168S.doi:10.1016/j.joule.2021.03.009.S2CID 233598665.
  23. ^"Speed of Sound in Water at Temperatures between 32–212 oF (0–100 oC) — imperial and SI units".The Engineering Toolbox.
  24. ^Wong, George S. K.; Zhu, Shi-ming (1995). "Speed of sound in seawater as a function of salinity, temperature, and pressure".The Journal of the Acoustical Society of America.97 (3): 1732.Bibcode:1995ASAJ...97.1732W.doi:10.1121/1.413048.
  25. ^APL-UW TR 9407 High-Frequency Ocean Environmental Acoustic Models Handbook, pp. I1-I2.
  26. ^Robinson, Stephen (22 September 2005)."Technical Guides – Speed of Sound in Sea-Water".National Physical Laboratory. Archived fromthe original on 29 April 2017. Retrieved7 December 2016.
  27. ^"How Fast Does Sound Travel?".Discovery of Sound in the Sea. University of Rhode Island. Archived fromthe original on 20 May 2017. Retrieved30 November 2010.
  28. ^abDushaw, Brian D.; Worcester, P. F.; Cornuelle, B. D.; Howe, B. M. (1993). "On Equations for the Speed of Sound in Seawater".Journal of the Acoustical Society of America.93 (1):255–275.Bibcode:1993ASAJ...93..255D.doi:10.1121/1.405660.
  29. ^Kenneth V., Mackenzie (1981). "Discussion of sea-water sound-speed determinations".Journal of the Acoustical Society of America.70 (3):801–806.Bibcode:1981ASAJ...70..801M.doi:10.1121/1.386919.
  30. ^Del Grosso, V. A. (1974)."New equation for speed of sound in natural waters (with comparisons to other equations)".Journal of the Acoustical Society of America.56 (4):1084–1091.Bibcode:1974ASAJ...56.1084D.doi:10.1121/1.1903388.
  31. ^Meinen, Christopher S.; Watts, D. Randolph (1997)."Further Evidence that the Sound-Speed Algorithm of Del Grosso Is More Accurate Than that of Chen and Millero".Journal of the Acoustical Society of America.102 (4):2058–2062.Bibcode:1997ASAJ..102.2058M.doi:10.1121/1.419655.S2CID 38144335.
  32. ^Maurice, S.; Chide, B.; Murdoch, N.; Lorenz, R. D.; Mimoun, D.; Wiens, R. C.; Stott, A.; Jacob, X.; Bertrand, T.; Montmessin, F.; Lanza, N. L.; Alvarez-Llamas, C.; Angel, S. M.; Aung, M.; Balaram, J. (1 April 2022)."In situ recording of Mars soundscape".Nature.605 (7911):653–658.Bibcode:2022Natur.605..653M.doi:10.1038/s41586-022-04679-0.ISSN 1476-4687.PMC 9132769.PMID 35364602.

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