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Wave Properties — Diagnostic Tests

Unit Tests

UT-1: Electromagnetic Wave Properties

Question:

A plane electromagnetic wave in vacuum has an electric field amplitude of E0=48Vm1E_0 = 48\,\text{V}\,\text{m}^{-1} and frequency f=5.0×1014Hzf = 5.0 \times 10^{14}\,\text{Hz}.

(a) Calculate the wavelength, the magnetic field amplitude B0B_0, and the intensity of the wave.

(b) The wave is incident normally on a surface of area 0.010m20.010\,\text{m}^2. Calculate the radiation pressure on the surface if it is (i) perfectly absorbing and (ii) perfectly reflecting.

(c) Calculate the energy of a single photon of this radiation.

Take c=3.00×108ms1c = 3.00 \times 10^8\,\text{m}\,\text{s}^{-1}, ε0=8.85×1012Fm1\varepsilon_0 = 8.85 \times 10^{-12}\,\text{F}\,\text{m}^{-1}, μ0=4π×107Hm1\mu_0 = 4\pi \times 10^{-7}\,\text{H}\,\text{m}^{-1}, h=6.63×1034Jsh = 6.63 \times 10^{-34}\,\text{J}\,\text{s}.

Solution:

(a) Wavelength: λ=c/f=3.00×108/(5.0×1014)=6.0×107m=600nm\lambda = c/f = 3.00 \times 10^8/(5.0 \times 10^{14}) = 6.0 \times 10^{-7}\,\text{m} = 600\,\text{nm} (visible light, orange)

Magnetic field amplitude: B0=E0/c=48/(3.00×108)=1.60×107TB_0 = E_0/c = 48/(3.00 \times 10^8) = 1.60 \times 10^{-7}\,\text{T}

Intensity: I=12ε0cE02=0.5×8.85×1012×3.00×108×2304=0.5×8.85×1012×6.912×1011=3.06Wm2I = \frac{1}{2}\varepsilon_0 c E_0^2 = 0.5 \times 8.85 \times 10^{-12} \times 3.00 \times 10^8 \times 2304 = 0.5 \times 8.85 \times 10^{-12} \times 6.912 \times 10^{11} = 3.06\,\text{W}\,\text{m}^{-2}

Alternatively: I=E0B0/(2μ0)=48×1.60×107/(2×4π×107)=7.68×106/(2.513×106)=3.06Wm2I = E_0 B_0/(2\mu_0) = 48 \times 1.60 \times 10^{-7}/(2 \times 4\pi \times 10^{-7}) = 7.68 \times 10^{-6}/(2.513 \times 10^{-6}) = 3.06\,\text{W}\,\text{m}^{-2}

(b) Radiation pressure:

(i) Perfectly absorbing: P=I/c=3.06/(3.00×108)=1.02×108PaP = I/c = 3.06/(3.00 \times 10^8) = 1.02 \times 10^{-8}\,\text{Pa}

Force on surface: F=PA=1.02×108×0.010=1.02×1010NF = PA = 1.02 \times 10^{-8} \times 0.010 = 1.02 \times 10^{-10}\,\text{N}

(ii) Perfectly reflecting: P=2I/c=2.04×108PaP = 2I/c = 2.04 \times 10^{-8}\,\text{Pa}

Force: F=2.04×1010NF = 2.04 \times 10^{-10}\,\text{N}

(c) Ephoton=hf=6.63×1034×5.0×1014=3.32×1019J=2.07eVE_{\text{photon}} = hf = 6.63 \times 10^{-34} \times 5.0 \times 10^{14} = 3.32 \times 10^{-19}\,\text{J} = 2.07\,\text{eV}


UT-2: Intensity and Amplitude Relationship

Question:

Two coherent sources S1S_1 and S2S_2 emit waves of wavelength λ=0.50m\lambda = 0.50\,\text{m} in phase. A point PP is located 4.0m4.0\,\text{m} from S1S_1 and 5.0m5.0\,\text{m} from S2S_2.

(a) Determine whether point PP is at a maximum, minimum, or neither, and calculate the ratio of the amplitude at PP to the amplitude from a single source.

(b) If the amplitude from each source alone at PP is A0A_0, derive the general expression for the amplitude at PP in terms of the path difference Δx\Delta x.

(c) Calculate the ratio of the intensity at PP to the intensity from a single source alone.

Solution:

(a) Path difference: Δx=5.04.0=1.0m\Delta x = 5.0 - 4.0 = 1.0\,\text{m}

Δx/λ=1.0/0.50=2.0\Delta x/\lambda = 1.0/0.50 = 2.0

Since the path difference is an integer number of wavelengths (n=2n = 2), PP is at a maximum (constructive interference).

The amplitude at PP is A=2A0A = 2A_0 (double slit maximum).

(b) Phase difference: ϕ=LB2πΔxRB◆◆LBλRB\phi = \frac◆LB◆2\pi \Delta x◆RB◆◆LB◆\lambda◆RB◆

The resultant amplitude from two waves of amplitude A0A_0 with phase difference ϕ\phi:

A=LBA02+A02+2A02cosϕRB=A0LB2(1+cosϕ)RB=2A0cosLBϕRB◆◆LB2RBA = \sqrt◆LB◆A_0^2 + A_0^2 + 2A_0^2\cos\phi◆RB◆ = A_0\sqrt◆LB◆2(1 + \cos\phi)◆RB◆ = 2A_0\left|\cos\frac◆LB◆\phi◆RB◆◆LB◆2◆RB◆\right|

In terms of path difference: ϕ=2πΔx/λ\phi = 2\pi\Delta x/\lambda

A=2A0cosLBπΔxRB◆◆LBλRBA = 2A_0\left|\cos\frac◆LB◆\pi\Delta x◆RB◆◆LB◆\lambda◆RB◆\right|

(c) Intensity is proportional to amplitude squared: IA2I \propto A^2

IPI0=(2A0)2A02=4\frac{I_P}{I_0} = \frac{(2A_0)^2}{A_0^2} = 4

At a maximum, the intensity is four times the intensity from a single source.

At a minimum (Δx=(n+0.5)λ\Delta x = (n + 0.5)\lambda): A=0A = 0 and I=0I = 0.


UT-3: Polarisation and Malus's Law

Question:

Unpolarised light of intensity I0I_0 passes through two polarising filters. The first has its transmission axis vertical. The second is rotated by an angle θ\theta from the vertical.

(a) Calculate the intensity transmitted through both filters as a function of θ\theta.

(b) At what angle θ\theta is the transmitted intensity equal to I0/8I_0/8?

(c) A third polariser is inserted between the first two, with its transmission axis at 4545^\circ to the vertical. Calculate the transmitted intensity when θ=90\theta = 90^\circ.

Solution:

(a) After the first (vertical) polariser, the intensity is I0/2I_0/2 (unpolarised light loses half its intensity through any polariser).

After the second polariser (at angle θ\theta), by Malus's law:

I=I02cos2θI = \frac{I_0}{2}\cos^2\theta

(b) I02cos2θ=I08\frac{I_0}{2}\cos^2\theta = \frac{I_0}{8}

cos2θ=14cosθ=12θ=60\cos^2\theta = \frac{1}{4} \Rightarrow \cos\theta = \frac{1}{2} \Rightarrow \theta = 60^\circ

(c) First polariser (vertical): intensity =I0/2= I_0/2, polarised vertically.

Second polariser (at 4545^\circ): I2=I02cos245=I02×12=I04I_2 = \frac{I_0}{2}\cos^2 45^\circ = \frac{I_0}{2} \times \frac{1}{2} = \frac{I_0}{4}, polarised at 4545^\circ.

Third polariser (horizontal, θ=90\theta = 90^\circ from vertical): the angle between the 4545^\circ polarisation and horizontal is 4545^\circ.

I3=I04cos245=I04×12=I08I_3 = \frac{I_0}{4}\cos^2 45^\circ = \frac{I_0}{4} \times \frac{1}{2} = \frac{I_0}{8}

Without the middle polariser, at θ=90\theta = 90^\circ the transmitted intensity would be zero (crossed polarisers). The insertion of a third polariser at 4545^\circ allows light to pass through, demonstrating that polarisers project the electric field onto their transmission axis rather than simply blocking light.

Integration Tests

IT-1: Doppler Effect and EM Waves (with Superposition)

Question:

A galaxy is moving away from Earth at a speed of 3.0×106ms13.0 \times 10^6\,\text{m}\,\text{s}^{-1}. A spectral line of wavelength 656nm656\,\text{nm} (hydrogen alpha) is observed from this galaxy.

(a) Calculate the observed wavelength of this line. (Use the non-relativistic Doppler formula.)

(b) Calculate the percentage change in the observed frequency.

(c) A space probe approaching Jupiter at 2.0×104ms12.0 \times 10^4\,\text{m}\,\text{s}^{-1} transmits a radio signal at 8.4GHz8.4\,\text{GHz}. Calculate the frequency received by an observer on Jupiter.

Take c=3.00×108ms1c = 3.00 \times 10^8\,\text{m}\,\text{s}^{-1}.

Solution:

(a) For a source moving away from the observer:

LBΔλRB◆◆LBλRB=vc\frac◆LB◆\Delta\lambda◆RB◆◆LB◆\lambda◆RB◆ = \frac{v}{c} Δλ=LB3.0×106RB◆◆LB3.00×108RB×656=0.010×656=6.56nm\Delta\lambda = \frac◆LB◆3.0 \times 10^6◆RB◆◆LB◆3.00 \times 10^8◆RB◆ \times 656 = 0.010 \times 656 = 6.56\,\text{nm}

Observed wavelength: λ=656+6.56=662.56663nm\lambda' = 656 + 6.56 = 662.56 \approx 663\,\text{nm} (redshifted)

(b) f=c/λf = c/\lambda, so Δf/f=Δλ/λ=v/c=1.0%\Delta f/f = -\Delta\lambda/\lambda = -v/c = -1.0\%

The frequency decreases by 1.0%1.0\%.

(c) The probe approaches Jupiter, so the observed frequency is higher:

f=f(ccv)=8.4×109×LB3.00×108RB◆◆LB3.00×1082.0×104RBf' = f\left(\frac{c}{c - v}\right) = 8.4 \times 10^9 \times \frac◆LB◆3.00 \times 10^8◆RB◆◆LB◆3.00 \times 10^8 - 2.0 \times 10^4◆RB◆ =8.4×109×LB3.00×108RB◆◆LB2.9998×108RB=8.4×109×1.000067=8.4006×109Hz= 8.4 \times 10^9 \times \frac◆LB◆3.00 \times 10^8◆RB◆◆LB◆2.9998 \times 10^8◆RB◆ = 8.4 \times 10^9 \times 1.000067 = 8.4006 \times 10^9\,\text{Hz}

The shift is Δf=5.6×105Hz=560kHz\Delta f = 5.6 \times 10^5\,\text{Hz} = 560\,\text{kHz}.


IT-2: Standing Waves on a String (with Oscillations)

Question:

A string of length 0.80m0.80\,\text{m} and mass 4.0×103kg4.0 \times 10^{-3}\,\text{kg} is fixed at both ends and stretched to a tension of 25N25\,\text{N}.

(a) Calculate the speed of transverse waves on the string.

(b) Calculate the fundamental frequency and the frequencies of the next two harmonics.

(c) The string is plucked at its centre. Explain which harmonics are excited and calculate the wavelength of the fundamental mode.

Solution:

(a) Wave speed: v=LBT/μRBv = \sqrt◆LB◆T/\mu◆RB◆, where μ=m/l=4.0×103/0.80=5.0×103kgm1\mu = m/l = 4.0 \times 10^{-3}/0.80 = 5.0 \times 10^{-3}\,\text{kg}\,\text{m}^{-1}

v=LB25/(5.0×103)RB=5000=70.7ms1v = \sqrt◆LB◆25/(5.0 \times 10^{-3})◆RB◆ = \sqrt{5000} = 70.7\,\text{m}\,\text{s}^{-1}

(b) For a string fixed at both ends, fn=nv/(2l)f_n = nv/(2l):

Fundamental (n=1n = 1): f1=70.7/(2×0.80)=44.2Hzf_1 = 70.7/(2 \times 0.80) = 44.2\,\text{Hz}

Second harmonic (n=2n = 2): f2=2×44.2=88.4Hzf_2 = 2 \times 44.2 = 88.4\,\text{Hz}

Third harmonic (n=3n = 3): f3=3×44.2=132.6Hzf_3 = 3 \times 44.2 = 132.6\,\text{Hz}

(c) Plucking at the centre excites the odd harmonics (n=1,3,5,n = 1, 3, 5, \ldots) most strongly because the centre is an antinode for odd harmonics and a node for even harmonics. Even harmonics (n=2,4,n = 2, 4, \ldots) have a node at the centre, so plucking there does not excite them.

Fundamental wavelength: λ1=2l=1.60m\lambda_1 = 2l = 1.60\,\text{m}

The fundamental mode has one antinode at the centre and nodes at both ends.


IT-3: Seismic Waves Through Earth Layers (with Properties of Materials)

Question:

P-waves (longitudinal) travel through the Earth's crust at 6.0kms16.0\,\text{km}\,\text{s}^{-1} and through the mantle at 10.0kms110.0\,\text{km}\,\text{s}^{-1}. The crust is 35km35\,\text{km} thick. A P-wave is detected at a seismograph 200km200\,\text{km} from the epicentre.

(a) Calculate the time for the P-wave to reach the seismograph via the direct path through the crust only.

(b) The wave refracts at the crust-mantle boundary. Using Snell's law, calculate the critical angle and determine whether total internal reflection occurs for the direct path.

(c) Explain why S-waves (transverse) are not detected on the opposite side of the Earth from a large earthquake.

Solution:

(a) Direct path through crust: t=d/vcrust=200/6.0=33.3st = d/v_{\text{crust}} = 200/6.0 = 33.3\,\text{s}

(b) The wave travels from crust (slower) into mantle (faster), so it bends away from the normal.

Critical angle (for TIR from mantle to crust):

sinθc=LBvcrustRB◆◆LBvmantleRB=6.010.0=0.60\sin\theta_c = \frac◆LB◆v_{\text{crust}}◆RB◆◆LB◆v_{\text{mantle}}◆RB◆ = \frac{6.0}{10.0} = 0.60 θc=36.9\theta_c = 36.9^\circ

For the direct path, the wave enters the mantle at some angle. Since the wave goes from a slower medium (crust) to a faster medium (mantle), TIR cannot occur at this boundary. TIR only occurs when going from a slower medium to a faster medium if the wave is already inside the slower medium -- which is not the case here. The wave always enters the mantle (it refracts away from the normal).

For a wave travelling through the mantle and hitting the crust-mantle boundary from below (trying to exit to the crust), TIR occurs at angles exceeding θc=36.9\theta_c = 36.9^\circ from the normal.

(c) S-waves are transverse and cannot propagate through liquids. The Earth's outer core is liquid, so S-waves are blocked by it. This creates an S-wave shadow zone on the opposite side of the Earth. The detection of this shadow zone was key evidence for the existence of a liquid outer core.