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Physics

Sound Waves

Pressure and Displacement Waves

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⚡ Quick Summary
Sound waves can be described by both displacement and pressure variations. Displacement is how much particles move from their original position, while pressure is the change in pressure due to the wave. These two descriptions are related but differ in phase by π/2, meaning pressure is maximum where displacement is zero, and vice versa.
p₀ = Bks₀, where p₀ is pressure amplitude, B is bulk modulus, k is wave number, and s₀ is displacement amplitude
The displacement wave is given by s = s₀ sin ω(t - x/v). The change in volume ΔV of an element due to the displacement is ΔV = -A s₀ ω cos ω(t - x/v)Δx / v, where A is the cross-sectional area. The stress (excess pressure) developed is p = -B(ΔV/V) = B (s₀ ω / v) cos ω(t - x/v), where B is the bulk modulus. The pressure amplitude p₀ and the displacement amplitude s₀ are related as p₀ = Bks₀, where k is the wave number. The pressure wave and displacement wave differ in phase by π/2. The human ear responds to pressure changes, making the pressure wave description more appropriate for sound detection.

Speed of a Sound Wave in a Material Medium

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⚡ Quick Summary
The speed of a sound wave in a fluid is determined by the properties of the medium, specifically its bulk modulus and density. We can derive the formula for the speed of sound by considering the forces on a small element of the fluid due to pressure differences.
Consider a sound wave described by displacement s = s₀ sin ω(t - x/v) and pressure p = (B s₀ ω / v) cos ω(t - x/v). For an element of fluid between x and x + Δx, the net force ΔF is given by ΔF = -A Δp = -A (B s₀ ω / v) (ω/v) Δx sin ω(t - x/v) = - (B s₀ ω² / v²) A Δx sin ω(t - x/v).

Speed of Sound in a Medium

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⚡ Quick Summary
The speed of sound depends on the elastic and inertial properties of the medium. For longitudinal waves, it relates to how easily the medium compresses or expands (elasticity) and how resistant it is to acceleration (inertia, represented by density).
['v = √(B/ρ)', 'Where:\nv = velocity of sound\nB = Bulk modulus of the medium\nρ = density of the medium']
  • The velocity of a longitudinal wave in a medium depends on its elastic properties and inertia properties.

Speed of Sound in Solids

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⚡ Quick Summary
Sound waves can travel through solid materials, and the speed is determined by the Young's modulus (a measure of stiffness) and the density of the solid.
['v = √(Y/ρ)', "Where:\nv = velocity of sound in the solid\nY = Young's modulus of the solid\nρ = density of the solid"]
  • The speed of longitudinal sound waves in a solid rod depends on its Young's modulus and its density.

Speed of Sound in a Gas: Newton's Formula

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⚡ Quick Summary
Newton initially proposed that sound propagation in a gas is an isothermal process (constant temperature). Based on this, he derived a formula for the speed of sound using Boyle's law (PV = constant).
['PV = constant (Isothermal Process)', 'B = -ΔP / (ΔV/V) = P', 'v = √(P/ρ)', 'Where:\nv = velocity of sound in the gas\nP = pressure of the gas\nρ = density of the gas']
  • Newton assumed that when a sound wave propagates through a gas, the temperature remains constant (isothermal conditions).
  • Boyle's law (PV = constant) is applicable in isothermal processes.

Speed of Sound in a Gas: Laplace's Correction

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⚡ Quick Summary
Laplace corrected Newton's formula by arguing that sound propagation is adiabatic (no heat exchange), not isothermal. This is because compressions and rarefactions happen too quickly for heat to dissipate. He used the adiabatic relation PV^γ = constant to derive a more accurate formula.
['PV<sup>γ</sup> = constant (Adiabatic Process)', 'γ = Cp/Cv', 'B = -ΔP / (ΔV/V) = γP', 'v = √(γP/ρ)', 'Where:\nv = velocity of sound in the gas\nγ = adiabatic index (ratio of specific heats)\nP = pressure of the gas\nρ = density of the gas']
  • Laplace suggested that compression and rarefaction occur rapidly, making the process adiabatic.

Speed of Sound

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⚡ Quick Summary
The speed of sound in a gas depends on the ratio of specific heats (γ), pressure (P), and density (ρ) of the gas. It is also affected by temperature and humidity.
['v = √(γP/ρ)', 'v = √(γcT)', 'v ∝ √T', 'v = v₀√( (273+t) / 273 )', 'v ≈ v₀(1 + t/546)']
  • The speed of sound is given by v = √(γP/ρ).
  • For air, γ ≈ 1.4. At STP, the speed of sound in air is approximately 332 m/s.
  • Pressure: If temperature is constant, changes in pressure do not affect the speed of sound.
  • Temperature: The speed of sound is proportional to the square root of the absolute temperature (v ∝ √T). The relationship can be approximated as v = v₀√( (273+t) / 273 ) ≈ v₀(1 + t/546), where v₀ is the speed of sound at 0°C and t is the temperature in °C.
  • Humidity: The speed of sound increases with increasing humidity because moist air is less dense than dry air.

Intensity of Sound Waves

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⚡ Quick Summary
Intensity of a sound wave is the average energy or power transmitted per unit area perpendicular to the direction of wave propagation. It's related to loudness and depends on the square of the pressure amplitude.
['p₀ = (Bωs₀)/v', 'W = (pA)(∂s/∂t)', 'I = (1/2) (p₀²v)/B', 'I = (1/2) p₀² / (ρv)', 'I = p₀² / (2ρv)']
  • Definition: Intensity (I) is the average energy crossing a unit area perpendicular to the direction of propagation per unit time or the average power transmitted across a unit area.
  • Loudness: The loudness of sound is mainly related to the intensity.
  • Equations: Given displacement s = s₀ sin ω(t - x/v) and excess pressure p = p₀ cos ω(t - x/v), where p₀ = (Bωs₀)/v.
  • Power transmitted: W = (pA)(∂s/∂t) = Ap₀ωs₀ cos²ω(t - x/v).
  • Intensity: I = (1/2) (Aω²s₀²B)/v = (1/2) s₀²ν²(2π²B)/v = p₀²v / (2B) = p₀² / (2ρv), where B is the bulk modulus, ρ is the density, and v is the speed of sound.

Sound Levels and Intensity

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⚡ Quick Summary
Sound intensity is measured in decibels (dB) using a logarithmic scale. The sound level is related to the intensity of the sound and a reference intensity. The appearance of sound is characterized by pitch, loudness and quality.
β = 10 log<sub>10</sub>(I/I<sub>0</sub>)
  • Sound Level (dB): The sound level (β) is measured in decibels and is defined as: β = 10 log10(I/I0), where I is the intensity of the sound and I0 is a constant reference intensity (10-12 W/m2).
  • Appearance of Sound:
    • Pitch: Sensation related to the dominant frequency of the sound. Higher frequency corresponds to higher pitch.
    • Loudness: Related to the intensity of the sound, better correlated with the sound level in decibels.
    • Quality: Related to the waveform of the sound wave, influenced by the different frequency components and their amplitudes.

Intensity and Pressure Amplitude

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⚡ Quick Summary
Intensity of a sound wave is proportional to the square of the pressure amplitude.
I' / I = (p'<sub>0</sub> / p<sub>0</sub>)<sup>2</sup>
The intensity (I) of a sound wave is proportional to the square of the pressure amplitude (p0). Therefore, if the pressure amplitude changes, the intensity changes proportionally to the square of the ratio of the pressure amplitudes.

Interference of Sound Waves

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⚡ Quick Summary
When two or more sound waves meet in the same area, they combine. Depending on how their peaks and valleys line up, they can either boost each other (constructive interference) making the sound louder, or cancel each other out (destructive interference) making the sound quieter or even silent. For interference to be easily heard, the sound sources need to be coherent, meaning they keep a constant phase relationship.
['Phase difference: δ = (2π/λ) * Δx', 'Constructive interference condition: δ = 2nπ or Δx = nλ', 'Destructive interference condition: δ = (2n + 1)π or Δx = (n + 1/2)λ', 'Resultant amplitude: p0^2 = p01^2 + p02^2 + 2 * p01 * p02 * cos(δ)', 'tan ε = (p02 * sin δ) / (p01 + p02 * cos δ)', 'Phase difference with initial phase difference: δ = δ0 + kΔx = δ0 + (2π/λ)Δx']

Interference of Sound Waves

The principle of superposition is valid for sound waves. The resultant disturbance is the sum of the individual disturbances.

Constructive Interference: Waves interfere constructively when their phase difference results in an increased intensity.

Destructive Interference: Waves interfere destructively when their phase difference results in a decreased intensity.

It's important to express waves in terms of pressure change when discussing interference.

Coherent Sources: Two sources whose phase difference remains constant in time.

Incoherent Sources: Sources with a phase difference that varies rapidly and randomly with time. No interference effect is observed.

For observable interference, sources must be coherent.

Interference of Sound Waves

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⚡ Quick Summary
Sound waves can interfere with each other. When sound waves are divided and travel along different paths before being recombined, they can either constructively or destructively interfere depending on the difference in the path lengths. Quinke's apparatus demonstrates this principle.
Phase difference due to path difference: δ = (2π/λ) * Δx
Interference of sound waves occurs when dividing the original wave along two different paths and then combining them. The two waves differ in phase due to the different path lengths traveled. A popular demonstration is the Quinke’s apparatus, where sound travels through two tubes of different lengths, recombines, and the resultant sound is detected. The intensity at the detector will be a maximum or a minimum depending on whether the difference in path lengths is an integral multiple of the wavelength or a half-wave integral multiple.

Reflection of Sound Waves

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⚡ Quick Summary
Sound waves reflect when they encounter a change in medium. Reflection from a rigid boundary causes a phase change in displacement (zero displacement), but pressure wave has same phase. Reflection from an open end causes a phase change of π in the pressure wave.
N/A
When there is a discontinuity in the medium, a sound wave gets reflected. Reflection from a rigid boundary: Particles at the boundary are unable to vibrate, so a reflected wave is generated that interferes with the oncoming wave to produce zero displacement at the boundary. The pressure variation is maximum at these points. A compression pulse reflects as a compression pulse, and a rarefaction pulse reflects as a rarefaction pulse. Reflection from a low-pressure region (e.g., open end of a tube): The particles vibrate with increased amplitude, and the pressure remains at the average value. The reflected pressure wave interferes destructively with the oncoming wave, resulting in a phase change of π. A compression pulse reflects as a rarefaction pulse, and vice versa.

Standing Longitudinal Waves and Vibrations of Air Columns

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⚡ Quick Summary
Standing waves can be produced by two identical longitudinal waves moving in opposite directions. The resultant wave is a standing wave.
p1 = p0 sin (ωt - kx) p2 = p0 sin (ωt + kx) p = p1 + p2 = 2p0 cos(kx) sin(ωt)
Standing waves are produced when two longitudinal waves of the same frequency and amplitude travel through a medium in opposite directions. The resultant wave is given by the superposition of the two waves, which leads to an equation similar to that of standing waves on a string.

Longitudinal Standing Waves

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In longitudinal standing waves, pressure amplitudes vary. Points of average pressure are pressure nodes, while points of maximum amplitude are pressure antinodes. Node-to-node or antinode-to-antinode distance is λ/2. Pressure nodes are displacement antinodes, and vice versa.
λ = (2n + 1)l/4 n = v/λ = (2n + 1)v/4l
Longitudinal standing waves exhibit variations in pressure amplitudes throughout the medium. Pressure nodes are points where the pressure remains at its average value, while pressure antinodes are points where the pressure amplitude is maximum. The distance between two consecutive nodes or antinodes is λ/2. A pressure node corresponds to a displacement antinode, and a pressure antinode corresponds to a displacement node.

Closed Organ Pipe

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⚡ Quick Summary
Closed organ pipes (cylindrical tubes closed at one end) produce standing waves at specific resonant frequencies. The closed end is a pressure antinode (displacement node), and the open end is a pressure node (displacement antinode). Only odd harmonics are present.
l = (2n + 1)λ/4 n = (2n + 1)v/4l n0 = v/4l
A closed organ pipe is a cylindrical tube with one end closed. Sound waves entering the open end are reflected from the closed end and again at the open end. The reflected waves interfere with incoming waves, leading to standing waves at resonant frequencies. The closed end is always a pressure antinode (displacement node), and the open end is a pressure node (displacement antinode). The condition for standing waves is l = (2n + 1)λ/4, where n = 0, 1, 2,... The fundamental frequency (n=0) is n0 = v/4l. Only odd harmonics are present in a closed organ pipe.

Resonance Column Method for Determining Speed of Sound

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⚡ Quick Summary
The resonance column method uses a tube, water, and a tuning fork to find the speed of sound. By adjusting the water level in the tube, we find lengths where the sound is loudest (resonance). These lengths relate to the wavelength of the sound, which we use to calculate the speed of sound.
['l₁ + d = λ/4 (First Resonance)', 'l₂ + d = 3λ/4 (Second Resonance)', 'λ = 2(l₂ - l₁) (Wavelength)', 'v = νλ = 2ν(l₂ - l₁) (Speed of Sound)', 'd = (l₂ - 3l₁)/2 (End Correction)']

Resonance Column Method

The resonance column method is used to measure the speed of sound in air using a long cylindrical glass tube (resonance tube), a water reservoir, and a tuning fork of known frequency.

Procedure:

  1. A tuning fork of known frequency (ν) is vibrated near the open end of the resonance tube.
  2. The water level in the tube is adjusted to change the length of the air column.
  3. When the air column resonates with the tuning fork, the loudness of the sound is maximum.
  4. The lengths of the air column corresponding to the first and second resonances (l1 and l2) are measured.

Theory:

  1. At the closed end (water surface), a pressure antinode is formed.
  2. At the open end, a pressure node is formed, but slightly above the open end due to end correction (d).
  3. For the first resonance (fundamental mode): l1 + d = λ/4
  4. For the second resonance (first overtone): l2 + d = 3λ/4

By subtracting the equations for first and second resonances, the wavelength (λ) can be determined:

(l2 + d) - (l1 + d) = 3λ/4 - λ/4

l2 - l1 = λ/2

λ = 2(l2 - l1)

The speed of sound (v) can then be calculated using the formula:

v = νλ

v = 2ν(l2 - l1)

End Correction: The end correction (d) accounts for the fact that the pressure node is not formed exactly at the open end of the tube. It can be calculated using the formula:

d = (l2 - 3l1)/2

Speed of Sound Measurement - Resonance Column Method

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⚡ Quick Summary
The speed of sound in air can be determined using the resonance column method by finding the wavelength of sound and multiplying it by the frequency of the tuning fork.
['v = νλ = 2(l₂ - l₁)ν']
The frequency of the wave is the same as the frequency of the tuning fork. The speed of sound is calculated as v = νλ = 2(l₂ - l₁)ν, where l₂ and l₁ are the lengths of the air column at resonance and ν is the frequency.

Speed of Sound Measurement - Kundt’s Tube Method

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⚡ Quick Summary
Kundt's tube method measures the speed of sound in a gas or solid by creating standing waves in a tube and measuring the distance between nodes of the wave pattern.
['λ = 2Δl', 'v = νλ = 2Δlν', 'v/va = l/Δl', 'v = va * (l/Δl)']
A gas is enclosed in a tube. A rod is vibrated longitudinally, creating standing waves in the gas. Powder in the tube collects at displacement nodes. The wavelength is twice the distance between successive heaps (λ = 2Δl). The speed of sound in the gas is v = νλ = 2Δlν. If the frequency is unknown, air is used as a reference. For solids, the ratio of speeds is v/va = l/Δl, where v is the speed in the solid, va is the speed in air, l is the length of the rod, and Δl is the distance between powder heaps in the air.

Beats

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Beats occur when two sound waves with slightly different frequencies superpose, resulting in periodic variations in amplitude.
['p = p₁ + p₂ = 2p₀ cos[((ω₁ - ω₂)/2)(t - x/v)] sin[((ω₁ + ω₂)/2)(t - x/v)]', 'Δω = |ω₁ - ω₂|']
Two sound waves with equal amplitudes and slightly different frequencies (ω₁ and ω₂) traveling in the same direction will superpose. The resultant pressure change is p = p₁ + p₂ = 2p₀ cos[((ω₁ - ω₂)/2)(t - x/v)] sin[((ω₁ + ω₂)/2)(t - x/v)]. Here Δω = |ω₁ - ω₂|.

Beats

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When two sound waves with slightly different frequencies interfere, the resulting sound intensity varies periodically. This phenomenon is called beats. The beat frequency is the absolute difference between the frequencies of the two original waves.
['p = A sin(ωt - x/v)', 'A = 2p₀ cos(ω_D/2 * t - x/v)', 'ω = (ω₁ + ω₂)/2', 'ω_D = ω₁ - ω₂', 'Beat frequency = |n₁ - n₂|']
When two sound waves of slightly different frequencies (ω₁ and ω₂) interfere, the resultant pressure change can be described as: p = A sin(ωt - x/v) where A = 2p₀ cos(ω_D/2 * t - x/v), ω = (ω₁ + ω₂)/2, and ω_D = ω₁ - ω₂. The amplitude A varies slowly with time compared to the wave itself. The amplitude |A| oscillates between 0 and 2p₀. The frequency of this amplitude variation is ω_D / (4π). The frequency of the intensity variation (beats) is |n₁ - n₂|, where n₁ and n₂ are the frequencies of the original waves. One cycle of maximum and minimum intensity is counted as one beat.

Doppler Effect

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The Doppler effect describes the change in frequency of a sound wave perceived by an observer when the source of the sound and/or the observer are moving relative to each other.
['T = 1/ν', 'ν′ = (v + u)/v * ν (Observer moving towards stationary source)', 'ν′ = (v - u)/v * ν (Observer moving away from stationary source)', 'ν′ = v/(v - u) * ν (Source moving towards stationary observer)', 'ν′ = v/(v + u) * ν (Source moving away from stationary observer)', 'ν′ = (v + u₀) / (v - uₛ) * ν (General Doppler effect formula)']
When a sound source vibrates at a frequency ν, it emits compression pulses at regular intervals T = 1/ν. The observed frequency changes based on the relative motion between the source and the observer. **Observer Moving Towards Stationary Source:** If the observer approaches a stationary source at a speed u, the apparent frequency is given by: ν′ = (v + u)/v * ν where: * ν′ is the apparent frequency. * ν is the original frequency. * v is the speed of sound in the medium. * u is the speed of the observer towards the source. **Observer Moving Away From Stationary Source:** If the observer recedes from a stationary source at a speed u, the apparent frequency is given by: ν′ = (v - u)/v * ν **Source Moving Towards Stationary Observer:** If the source approaches a stationary observer at a speed u, the apparent frequency is given by: ν′ = v/(v - u) * ν **Source Moving Away From Stationary Observer:** If the source recedes from a stationary observer at a speed u, the apparent frequency is given by: ν′ = v/(v + u) * ν **General Formula:** A general formula encompassing all scenarios is: ν′ = (v + u₀) / (v - uₛ) * ν where: * u₀ is the speed of the observer with respect to the medium (positive when moving towards the source, negative when moving away). * uₛ is the speed of the source with respect to the medium (positive when moving towards the observer, negative when moving away). Important Considerations: * Speeds u₀ and uₛ must be measured with respect to the medium carrying the sound. * If the medium itself is moving, appropriate calculations are needed to find the speeds of the source and observer relative to the medium.

Mach Number

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The Mach number is the ratio of the speed of a source to the speed of sound in the medium.
Mach Number = s/v

The ratio of the speed of the source (s) to the speed of sound (v) is called the Mach Number.

Sonic Boom

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A sonic boom is the loud sound produced when an object travels faster than the speed of sound. It's a continuous effect as long as the object maintains supersonic speed.
N/A

When an observer on the ground is intercepted by the cone surface (created by a supersonic object), the boom is heard.

The sonic boom is not a one-time affair but continues as long as the plane moves with supersonic speed.

Musical Scale (Diatonic)

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A musical scale is a sequence of frequencies that sound pleasing. The diatonic scale is a common one with eight notes covering an octave.
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A musical scale is a sequence of frequencies which have a particularly pleasing effect on the human ear.

A widely used musical scale, called diatonic scale, has eight frequencies covering an octave. Each frequency is called a note.

Acoustics of Buildings

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Acoustics in buildings involves managing sound reflection and absorption to ensure clarity and loudness. Echoes and reverberation need to be controlled.
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While designing an auditorium, one has to take care of absorption and reflection of sound for clear audibility.

Reflection of sound helps in maintaining loudness but also causes unwanted effects like echoes and reverberation.

Reverberation can be decreased by using sound-absorbing materials.

An auditorium with a very small reverberation time is called acoustically dead.

Reverberation Time

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Reverberation time is the time it takes for the intensity of a reverberant sound to decrease significantly. It's crucial for good acoustics.
Reverberation time: Time for intensity to decrease by a factor of 10^6

Reverberation is the effect of multiple reflections where sound signals arrive in quick succession with decreasing intensity.

The time taken by the reverberant sound to decrease its intensity by a factor of 106 is called the reverberation time.

Electrical Amplifying Systems and Auditorium Acoustics

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Electrical amplifying systems in large auditoriums can cause feedback (ringing) if the loudspeaker is near the microphone. Sound from loudspeakers should reach listeners simultaneously with sound from the stage, using proper inclinations and electronic delays. Noise from outside or equipment inside the auditorium should be minimized.
N/A
Electrical amplifying systems are often used in large auditoriums. If a loudspeaker is kept near the microphone, the amplifying system may pick up sound from the loudspeaker to again amplify it. This gives a very unpleasant whistling sound. One also has to avoid any noise coming from outside the auditorium or from different equipment inside the auditorium. Sound of fans, exhausts, air conditioners, etc., often create annoyance to the listener. Loudspeakers are placed with proper inclinations and electronic delays are installed so that sound from the stage and from the loudspeaker reach a listener almost simultaneously.

Speed of Sound and Wavelength

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⚡ Quick Summary
The speed of sound is related to the frequency and wavelength of the sound wave by the formula v = λν.
v = λν
The speed of sound (v) is related to the frequency (ν) and wavelength (λ) of the sound wave.

Sound Wave Equation

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⚡ Quick Summary
The general equation for a sound wave is p = p0 sin(ωt - kx), where p is the pressure, p0 is the pressure amplitude, ω is the angular frequency, t is time, k is the wave number, and x is the position.
p = p0 sin(ωt - kx) ω = 2πν k = 2π/λ
The equation of a sound wave is generally given as p = p0 sin(ωt - kx), where: * p is the pressure at a given point and time. * p0 is the pressure amplitude. * ω is the angular frequency (ω = 2πν). * t is time. * k is the wave number (k = 2π/λ). * x is the position.

Phase Difference and Separation

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The phase difference between two points in a wave is related to the wave number and the separation between the points by ΔΦ = kΔx.
ΔΦ = kΔx k = 2π/λ
The phase difference (ΔΦ) between two points in a wave is given by ΔΦ = kΔx, where: * k is the wave number (k = 2π/λ). * Δx is the separation between the two points.

Speed of Sound and Intensity

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The speed of sound in a gas depends on the temperature and the gas's properties. Intensity of a sound wave is related to the amplitude of the air particle's vibration.
['v ∝ √T', 'I = 2π<sup>2</sup>s<sub>0</sub><sup>2</sup>ν<sup>2</sup>ρv', 'β = 10 log<sub>10</sub>(I/I<sub>0</sub>)', 'p ∝ √I']
  • The speed of sound is proportional to the square root of the absolute temperature.
  • The intensity of sound and the displacement amplitude is related by: I = 2π2s02ν2ρv where I is intensity, s0 is displacement amplitude, ν is frequency, ρ is density, and v is speed.
  • The sound level in dB is β = 10 log10(I/I0).
  • Intensity is proportional to the square of the pressure amplitude.

Frequency and Tension in a String

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The frequency of vibration of a string increases with an increase in tension.
N/A
The frequency of vibration of a string increases with increase in the tension. Thus, the note emitted by the string will be a little more than 440 Hz.

Doppler Effect

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The apparent frequency changes when there's relative motion between the source and the observer.
ν′ = ν * (v / (v + us)) [Source moving away] ν′′ = ν * (v / (v - us)) [Source moving towards]
When a sound source moves relative to an observer, the apparent frequency heard by the observer changes. The Doppler effect formulas are used to calculate this change in frequency based on the speeds of the source and observer relative to the medium.

Fundamental Frequency of Organ Pipe

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The fundamental frequency of an organ pipe depends on the speed of sound in the gas it contains.
500 / ν = v_a / v_h = sqrt(ρ_h / ρ_a)
The fundamental frequency of an organ pipe is proportional to the speed of sound in the gas contained within it.

Speed of Sound in a Solid Rod

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The speed of sound in a solid rod depends on the Young's modulus and density of the material.
v = sqrt(Y / ρ)
The speed of sound in a solid rod is determined by the material's Young's modulus (Y) and its density (ρ).

Longitudinal Vibrations in a Rod Clamped at the Middle

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When a rod is clamped at the middle and vibrates in its fundamental mode, the middle point is a pressure antinode, and the ends are nodes.
λ = 2l
When a rod is clamped at its middle point and set into longitudinal vibrations in its fundamental mode: The middle point is a pressure antinode. The free ends of the rod are nodes. The length of the rod is equal to half the wavelength.

Doppler Effect

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The Doppler effect is the change in frequency of a sound wave perceived by an observer due to the relative motion between the source and the observer.
ν' = ν / (1 - (u cos θ) / v)
When a source is approaching a stationary observer, the frequency heard by the observer is higher than the actual frequency of the source. The formula for the apparent frequency (ν') when the source is moving towards a stationary observer is: ν' = ν / (1 - (u cos θ) / v), where ν is the original frequency, v is the speed of sound, u is the speed of the source, and θ is the angle between the direction of the source's motion and the line connecting the source and the observer.

Sound Wave Properties and Medium

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Sound waves are affected by the properties of the medium they travel through. Elasticity and inertia are key factors influencing the speed of sound. Frequency remains unchanged during refraction.
Sound waves involve oscillations in pressure and displacement of the medium. The speed of sound in a medium depends on both its elastic properties (e.g., bulk modulus) and its inertial properties (e.g., density). During refraction from one medium to another (e.g., air to water), the frequency of the sound wave remains unchanged, while wavelength and wave velocity change. When two waves with the same frequency and constant phase difference interfere, there is no gain or loss of energy; energy is redistributed.

Power of Sound Waves

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The average power transmitted by a sound wave is related to its pressure amplitude and wavelength. Changes in wavelength affect the power transmitted.
The average power transmitted across a cross-section by a sound wave depends on its pressure amplitude and wavelength. If two sound waves move in the same direction with equal pressure amplitudes but different wavelengths, the wave with twice the wavelength will transmit four times the power.

Speed of Sound

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The speed of sound depends on the properties of the medium it travels through.
v = √(γRT/M), where v is the speed of sound, γ is the adiabatic index, R is the gas constant, T is the absolute temperature, and M is the molar mass.
The speed of sound in a gas depends on the temperature of the gas. It increases with temperature.

Wavelength and Frequency

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The wavelength and frequency of a sound wave are related to its speed.
v = fλ, where v is the speed of sound, f is the frequency, and λ is the wavelength.
The speed of sound (v) is related to the wavelength (λ) and frequency (f) by the equation v = fλ.

Bulk Modulus

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Bulk modulus relates pressure change to volume change.
B = -ΔP/(ΔV/V), where B is the bulk modulus, ΔP is the change in pressure, ΔV is the change in volume, and V is the original volume.
Bulk modulus (B) is a measure of a substance's resistance to compression. It relates the change in pressure to the fractional change in volume.

Intensity of Sound

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Sound intensity measures the power of sound per unit area.
I = P/A, where I is the intensity, P is the power, and A is the area. For a point source: I ∝ 1/r², where r is the distance from the source.
Intensity (I) is the power (P) of the sound wave per unit area (A). For a point source, the intensity decreases with the square of the distance from the source.

Sound Level (Decibels)

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Sound level in decibels (dB) is a logarithmic measure of sound intensity relative to a reference intensity.
β = 10 log₁₀(I/I₀), where β is the sound level in dB, I is the intensity, and I₀ is the reference intensity.
The sound level (β) in decibels is defined as β = 10 log₁₀(I/I₀), where I is the intensity of the sound and I₀ is the reference intensity (usually 10⁻¹² W/m²).

Quincke's Tube

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Quincke's tube demonstrates interference of sound waves.
Path difference = nλ (constructive interference, maximum intensity), Path difference = (n + 1/2)λ (destructive interference, minimum intensity), where n is an integer and λ is the wavelength.
In Quincke's tube experiment, the path difference between two sound waves leads to constructive or destructive interference, resulting in maximum or minimum sound intensity.

Constructive Interference

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Constructive interference occurs when waves from different sources arrive at a point in phase, resulting in a higher intensity than either wave alone.
Path difference = nλ, where n is an integer (0, 1, 2, ...)
When two sources of sound vibrate at the same frequency and are in phase, the intensity of the resulting sound wave depends on the path difference between the waves from the two sources. Constructive interference occurs when the path difference is an integer multiple of the wavelength.

Open Organ Pipe

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An open organ pipe is open at both ends. It can resonate at frequencies that are integer multiples of the fundamental frequency.
f_n = n * (v / 2L), where n = 1, 2, 3,... f_n is the frequency of the nth harmonic, v is the speed of sound, and L is the length of the pipe.
An open organ pipe has antinodes at both ends. The fundamental frequency (first harmonic) corresponds to a wavelength twice the length of the pipe. The higher harmonics are integer multiples of the fundamental frequency.

Closed Organ Pipe

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A closed organ pipe is closed at one end and open at the other. It resonates at frequencies that are odd integer multiples of the fundamental frequency.
f_n = n * (v / 4L), where n = 1, 3, 5,... f_n is the frequency of the nth harmonic, v is the speed of sound, and L is the length of the pipe.
A closed organ pipe has a node at the closed end and an antinode at the open end. The fundamental frequency corresponds to a wavelength four times the length of the pipe. Only odd harmonics are present.

Standing Waves in Air Column

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Standing waves in an air column are formed by the superposition of two waves traveling in opposite directions. Nodes are points of minimum displacement, and antinodes are points of maximum displacement.
Distance between node and antinode = λ/4
In a vibrating air column, nodes are formed where the displacement is minimum (zero), and antinodes are formed where the displacement is maximum. The distance between a node and the next antinode is one-quarter of the wavelength.

Resonance Column

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A resonance column is used to determine the speed of sound in air by finding the lengths of air columns that resonate with a tuning fork.
v = fλ, where v is the speed of sound, f is the frequency, and λ is the wavelength.
In a resonance column experiment, resonance occurs when the frequency of the tuning fork matches a natural frequency of the air column. The first resonance occurs when the length of the air column is approximately λ/4, and the second resonance occurs when the length is approximately 3λ/4.

Overtones and Harmonics

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Harmonics are integer multiples of the fundamental frequency. Overtones are the frequencies above the fundamental frequency.
f_n = n * f_1, where f_n is the frequency of the nth harmonic and f_1 is the fundamental frequency.
The fundamental frequency is the first harmonic. The first overtone is the second harmonic, the second overtone is the third harmonic, and so on. In an open pipe, all harmonics are present. In a closed pipe, only odd harmonics are present.

Standing Waves on a Wire

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Standing waves can be set up on a wire fixed at both ends. The frequencies of the standing waves depend on the length, tension, and mass per unit length of the wire.
f_n = n * (v / 2L), where n = 1, 2, 3,... f_n is the frequency of the nth harmonic, v is the speed of the wave on the wire, and L is the length of the wire. v = sqrt(T/μ), where T is the tension and μ is the mass per unit length.
When a wire is fixed at both ends, standing waves can be formed. The fundamental frequency (first harmonic) corresponds to a wavelength twice the length of the wire. The higher harmonics are integer multiples of the fundamental frequency.

Effect of Temperature on Frequency

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The frequency of an organ pipe changes with temperature due to the change in the speed of sound.
Δν/ν = ΔT/2T, where ν is the frequency, T is the temperature, and Δν and ΔT are the changes in frequency and temperature, respectively.
The speed of sound in air depends on the temperature. As the temperature increases, the speed of sound increases, and the frequency of the organ pipe also increases.

Doppler Effect

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The Doppler effect describes the change in frequency of a wave (like sound) when the source of the wave or the observer is moving. If they are moving closer, the frequency increases; if they are moving apart, the frequency decreases.
["f' = f (v + vo) / v (Observer moving towards source)", "f' = f (v - vo) / v (Observer moving away from source)", "f' = f v / (v - vs) (Source moving towards observer)", "f' = f v / (v + vs) (Source moving away from observer)"]
The Doppler effect is observed when the source of sound or the observer is in motion relative to the medium. The observed frequency (f') differs from the source frequency (f) depending on the velocities of the source (vs) and the observer (vo) relative to the speed of sound (v). The formulas for calculating the apparent frequency are as follows: * **Observer Moving Towards Source:** f' = f (v + vo) / v * **Observer Moving Away From Source:** f' = f (v - vo) / v * **Source Moving Towards Observer:** f' = f v / (v - vs) * **Source Moving Away From Observer:** f' = f v / (v + vs) Where: * f' = Observed frequency * f = Source frequency * v = Speed of sound in the medium * vo = Velocity of the observer * vs = Velocity of the source

Fundamental Frequency of Closed Pipe

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A closed pipe (one end closed, one end open) has a fundamental frequency, which is the lowest frequency at which it naturally vibrates. This frequency depends on the length of the pipe and the speed of sound.
['f = v / (4L) (Fundamental frequency of a closed pipe)', 'v = √(γRT/M) (Speed of sound in a gas, depends on Temperature)']
A closed pipe resonates at specific frequencies, with the fundamental frequency being the lowest. The fundamental frequency occurs when the length of the pipe (L) is equal to one-quarter of the wavelength (λ/4). Therefore, the wavelength of the fundamental mode is 4L. The fundamental frequency (f) is related to the speed of sound (v) and the wavelength (λ) by the equation v = fλ. Therefore, f = v/λ

Kundt's Tube

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Kundt's tube is an apparatus used to measure the speed of sound in a gas or a solid. A rod vibrates, creating sound waves in the tube, and powder inside the tube clumps together at nodes (points of no vibration). The distance between these nodes is related to the wavelength of the sound.
['v = fλ (Relationship between speed, frequency, and wavelength)', "λ = 2d (Wavelength from node distance in Kundt's tube)", 'v_rod = f * 2L (Speed of sound in rod if clamped at center)', 'v_rod = f * 4L (Speed of sound in rod if clamped at L/4 from end)']
Kundt's tube uses a vibrating rod to generate sound waves in a tube containing a powder (e.g., lycopodium). The sound waves create standing waves within the tube. The powder collects at the nodes of these standing waves, which are points of minimal displacement. The distance (d) between adjacent nodes is equal to half the wavelength (λ/2) of the sound wave in the air. If the rod is clamped at its center, the fundamental frequency is excited and the length of rod is half wavelength. If clamped at L/4 from end, the length of rod is one-fourth wavelength

Beats

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Beats are the periodic variations in sound intensity heard when two sound waves of slightly different frequencies interfere with each other. The beat frequency is equal to the difference in the frequencies of the two waves.
['fb = |f1 - f2| (Beat frequency)']
When two sound waves of slightly different frequencies (f1 and f2) are superimposed, the resulting sound has a periodic variation in amplitude, known as beats. The beat frequency (fb) is the absolute difference between the two frequencies: fb = |f1 - f2|

Frequency and Tension in a Wire

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The fundamental frequency of a vibrating wire depends on its tension. Increasing the tension increases the frequency.
['f1/f2 = √(T1/T2) (Relationship between frequency and tension)']
The fundamental frequency of a vibrating wire is directly proportional to the square root of the tension in the wire. If f1 and f2 are the frequencies corresponding to tensions T1 and T2, respectively, then: f1/f2 = √(T1/T2)

Doppler Effect

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The Doppler effect describes the change in frequency of a sound wave perceived by a listener when the source of the sound and the listener are in relative motion.
["f' = f (v ± vo) / (v ± vs)"]
The Doppler effect is a change in the observed frequency of a wave when the source or observer moves. **Formulas:** * **General Formula:** f' = f (v ± vo) / (v ± vs) where: * f' is the observed frequency * f is the source frequency * v is the speed of sound in the medium * vo is the speed of the observer * vs is the speed of the source Use +vo if the observer is moving towards the source, -vo if moving away. Use -vs if the source is moving towards the observer, +vs if moving away.

Beats

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Beats are the periodic variations in amplitude that occur when two sound waves of slightly different frequencies interfere with each other.
['Beat Frequency = |f1 - f2|']
When two sound waves of slightly different frequencies interfere, we hear beats. The beat frequency is equal to the difference in the frequencies of the two waves. **Formula:** Beat Frequency = |f1 - f2|

Wavelength

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Wavelength is the distance between two consecutive crests or troughs of a wave.
[]
Wavelength is the spatial period of a periodic wave—the distance over which the wave's shape repeats. It's often denoted by λ (lambda).

Doppler Effect

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The Doppler effect describes the change in frequency of a sound wave perceived by an observer when the source of the sound and the observer are in relative motion.
[{'name': 'Observed frequency when source is moving towards observer', 'formula': "f' = f * (v / (v - vs))", 'variables': {"f'": 'Observed frequency', 'f': 'Source frequency', 'v': 'Speed of sound in the medium', 'vs': 'Speed of the source'}}, {'name': 'Observed frequency when source is moving away from observer', 'formula': "f' = f * (v / (v + vs))", 'variables': {"f'": 'Observed frequency', 'f': 'Source frequency', 'v': 'Speed of sound in the medium', 'vs': 'Speed of the source'}}, {'name': 'Observed frequency when observer is moving towards source', 'formula': "f' = f * ((v + vo) / v)", 'variables': {"f'": 'Observed frequency', 'f': 'Source frequency', 'v': 'Speed of sound in the medium', 'vo': 'Speed of the observer'}}, {'name': 'Observed frequency when observer is moving away from source', 'formula': "f' = f * ((v - vo) / v)", 'variables': {"f'": 'Observed frequency', 'f': 'Source frequency', 'v': 'Speed of sound in the medium', 'vo': 'Speed of the observer'}}, {'name': 'General formula', 'formula': "f' = f * ((v + vo) / (v - vs))", 'variables': {"f'": 'Observed frequency', 'f': 'Source frequency', 'v': 'Speed of sound in the medium', 'vo': 'Velocity of observer (positive if moving towards source)', 'vs': 'Velocity of source (positive if moving towards observer)'}}]
The Doppler effect occurs whenever there is relative motion between a source of waves and an observer. When the source and the observer are moving towards each other, the observed frequency increases. When they are moving away from each other, the observed frequency decreases.

Doppler Effect (Implied from Problems)

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The Doppler effect describes the change in frequency of a sound wave perceived by an observer moving relative to the source of the sound.
['v = fλ (Speed of sound = frequency * wavelength)', "f' = f (v ± vo) / (v ± vs) (Doppler effect formula, where f' is observed frequency, f is source frequency, v is speed of sound, vo is observer speed, and vs is source speed. The signs depend on the direction of motion.)", 'Beat Frequency = |f1 - f2| (Absolute difference between two frequencies)', 'Resonance Frequencies for Open Pipes: f_n = n(v/2L), n = 1, 2, 3...', 'Resonance Frequencies for Closed Pipes: f_n = n(v/4L), n = 1, 3, 5...']
The provided text consists only of numerical answers to problems. Therefore, extracting detailed notes on theory, definitions, and formulas is impossible *from this text alone*. However, based on the types of answers given (frequencies, speeds, distances), we can infer that the problems likely involve the following concepts: * **Speed of Sound:** Calculations involving the speed of sound in different media (air, solids). Factors affecting the speed of sound (temperature). * **Frequency and Wavelength:** Relationship between frequency, wavelength, and speed of sound (v = fλ). * **Superposition of Waves:** Interference, beats. * **Resonance:** Standing waves in pipes (open and closed). * **Doppler Effect:** Change in frequency due to relative motion of source and observer.

Sound Waves

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Mechanical waves that propagate through a medium, creating compressions and rarefactions.
Speed of sound in a fluid: v = √(B/ρ); Speed of sound in a solid: v = √(Y/ρ); Beat frequency: |f1 - f2|; Doppler effect: f' = f((v ± vo)/(v ± vs))
Covers topics such as amplitude, frequency, wavelength, speed of sound, interference, beats, and the Doppler effect.

Doppler Effect

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The Doppler effect describes the change in frequency of a sound wave perceived by an observer when the source of the sound and the observer are in relative motion.
Observed frequency f' = f (v + vo) / (v - vs), where f is the source frequency, v is the speed of sound, vo is the observer's velocity (positive if approaching source), and vs is the source velocity (positive if approaching observer).
The Doppler effect occurs when a source of waves is moving relative to an observer. If the source is approaching, the observed frequency is higher than the emitted frequency. If the source is receding, the observed frequency is lower. The change in frequency depends on the speeds of the source and observer relative to the medium (air, in this case) carrying the sound.

Fundamental Frequency of Closed Pipe

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The fundamental frequency of a closed pipe is the lowest frequency at which it resonates. It depends on the length of the pipe and the speed of sound.
f = v / (4L), where f is the fundamental frequency, v is the speed of sound, and L is the length of the pipe.
A closed pipe (closed at one end) supports standing waves with a node at the closed end and an antinode at the open end. The fundamental frequency corresponds to a quarter-wavelength fitting inside the pipe length.

Kundt's Tube

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A Kundt's tube is used to measure the speed of sound in a solid. It relies on creating standing waves in both the solid and the air within the tube.
v = f * lambda, where v is the speed of sound, f is the frequency, and lambda is the wavelength (twice the distance between nodes).
Kundt's tube demonstrates resonance in a solid rod and the air within a tube. The solid rod is vibrated, producing sound waves in the air. The powder in the tube collects at the nodes of the standing wave pattern. By measuring the distance between the nodes and knowing the frequency, one can calculate the speed of sound in both the air and the solid rod.

Beats

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Beats are produced when two sound waves of slightly different frequencies interfere. The beat frequency is the difference between the two frequencies.
Beat frequency = |f1 - f2|, where f1 and f2 are the frequencies of the two sound waves.
When two sound waves with slightly different frequencies are played simultaneously, the resulting sound has a varying amplitude, creating a periodic variation in loudness called beats. The number of beats per second equals the difference in the frequencies of the two sound waves.

Frequency and Wavelength

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The speed of a wave is related to its frequency and wavelength.
v = f * lambda, where v is the speed of the wave, f is the frequency, and lambda is the wavelength.
The speed of a wave in a medium is related to the frequency and wavelength of the wave. Higher frequency waves have shorter wavelengths, and lower frequency waves have longer wavelengths, for a given speed.

Tuning Forks and Beats

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The beat frequency helps determine the unknown frequency of a tuning fork by comparing it to a known frequency and observing how the beat frequency changes when the tuning fork is slightly altered.
Beat frequency = |f1 - f2|, where f1 and f2 are the frequencies of the two tuning forks.
If loading a tuning fork (e.g., with wax) decreases its frequency, and this *decreases* the beat frequency relative to a known fork, then the original unknown frequency was *higher* than the known. Conversely, if loading decreases the tuning fork frequency, and this *increases* the beat frequency, then the original unknown frequency was *lower* than the known. This allows solving for the precise original frequency.

Wire Vibration

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The frequency of a vibrating wire depends on its length and tension. Changing the length or tension will change the frequency.
f ∝ √(T)/L, where f is frequency, T is tension, and L is length.
The fundamental frequency of a vibrating wire is directly proportional to the square root of the tension and inversely proportional to the length of the wire. If the tension is increased, the frequency increases, and if the length is increased, the frequency decreases. The number of beats produced per second is the difference in frequency between the vibrating wire and the tuning fork.